diff --git a/lib/__init__.py b/lib/__init__.py
index 0dbaa09..87832bf 100644
--- a/lib/__init__.py
+++ b/lib/__init__.py
@@ -22,7 +22,7 @@
 def parse_error(error):
     exc_type = type(error).__name__
     exc_obj = f"{error}".replace("\n", " ").replace("   ", " ")
-    return f"{exc_type} exception: {exc_obj}"
+    return f"{exc_type}: {exc_obj}"
 
 
 from lib.api import app
diff --git a/lib/controllers/flight.py b/lib/controllers/flight.py
index af2b307..901cddc 100644
--- a/lib/controllers/flight.py
+++ b/lib/controllers/flight.py
@@ -2,37 +2,22 @@
 from fastapi import HTTPException, status
 from pymongo.errors import PyMongoError
 
-from rocketpy.simulation.flight import Flight as RocketPyFlight
 
 import jsonpickle
 
 from lib import logger, parse_error
-from lib.models.rocket import Rocket, RocketOptions
-from lib.models.motor import MotorKinds
-from lib.models.flight import Flight
 from lib.models.environment import Env
+from lib.models.rocket import Rocket
+from lib.models.flight import Flight
 from lib.views.flight import (
     FlightSummary,
-    SurfaceWindConditions,
-    OutOfRailConditions,
-    BurnoutConditions,
-    ApogeeConditions,
-    MaximumValues,
-    InitialConditions,
-    NumericalIntegrationSettings,
-    ImpactConditions,
-    EventsRegistered,
-    LaunchRailConditions,
-    FlightData,
     FlightCreated,
     FlightUpdated,
     FlightDeleted,
     FlightPickle,
 )
 from lib.repositories.flight import FlightRepository
-from lib.controllers.environment import EnvController
-from lib.controllers.rocket import RocketController
-from lib.services.environment import EnvironmentService
+from lib.services.flight import FlightService
 
 
 class FlightController:
@@ -56,49 +41,17 @@ class FlightController:
     def __init__(
         self,
         flight: Flight,
-        *,
-        rocket_option: RocketOptions,
-        motor_kind: MotorKinds,
     ):
         self._flight = flight
-        self._rocket_option = rocket_option
-        self._motor_kind = motor_kind
 
     @property
     def flight(self) -> Flight:
         return self._flight
 
-    @property
-    def rocket_option(self) -> RocketOptions:
-        return self._rocket_option
-
-    @property
-    def motor_kind(self) -> MotorKinds:
-        return self._motor_kind
-
     @flight.setter
     def flight(self, flight: Flight):
         self._flight = flight
 
-    @staticmethod
-    def get_rocketpy_flight(flight: Flight) -> RocketPyFlight:
-        """
-        Get the rocketpy flight object.
-
-        Returns:
-            RocketPyFlight
-        """
-        rocketpy_rocket = RocketController.get_rocketpy_rocket(flight.rocket)
-        rocketpy_env = EnvironmentService.from_env_model(flight.environment)
-        rocketpy_flight = RocketPyFlight(
-            rocket=rocketpy_rocket,
-            inclination=flight.inclination,
-            heading=flight.heading,
-            environment=rocketpy_env,
-            rail_length=flight.rail_length,
-        )
-        return rocketpy_flight
-
     async def create_flight(self) -> Union[FlightCreated, HTTPException]:
         """
         Create a flight in the database.
@@ -109,10 +62,7 @@ async def create_flight(self) -> Union[FlightCreated, HTTPException]:
         try:
             async with FlightRepository() as flight_repo:
                 flight_repo.fetch_flight(self.flight)
-                await flight_repo.create_flight(
-                    motor_kind=self.motor_kind,
-                    rocket_option=self.rocket_option,
-                )
+                await flight_repo.create_flight()
         except PyMongoError as e:
             logger.error(f"controllers.flight.create_flight: PyMongoError {e}")
             raise HTTPException(
@@ -201,7 +151,7 @@ async def get_rocketpy_flight_as_jsonpickle(
         """
         try:
             read_flight = await cls.get_flight_by_id(flight_id)
-            rocketpy_flight = cls.get_rocketpy_flight(read_flight)
+            rocketpy_flight = FlightService.from_flight_model(read_flight)
         except HTTPException as e:
             raise e from e
         except Exception as e:
@@ -240,10 +190,7 @@ async def update_flight_by_id(
         try:
             async with FlightRepository() as flight_repo:
                 flight_repo.fetch_flight(self.flight)
-                await flight_repo.create_flight(
-                    motor_kind=self.motor_kind,
-                    rocket_option=self.rocket_option,
-                )
+                await flight_repo.create_flight()
                 await flight_repo.delete_flight_by_id(flight_id)
         except PyMongoError as e:
             logger.error(f"controllers.flight.update_flight: PyMongoError {e}")
@@ -291,10 +238,7 @@ async def update_env_by_flight_id(
             new_flight = Flight(**new_flight)
             async with FlightRepository() as flight_repo:
                 flight_repo.fetch_flight(new_flight)
-                await flight_repo.create_flight(
-                    motor_kind=read_flight.rocket.motor.motor_kind,
-                    rocket_option=read_flight.rocket.rocket_option,
-                )
+                await flight_repo.create_flight()
                 await flight_repo.delete_flight_by_id(flight_id)
         except PyMongoError as e:
             logger.error(
@@ -322,7 +266,7 @@ async def update_env_by_flight_id(
 
     @classmethod
     async def update_rocket_by_flight_id(
-        cls, flight_id: str, *, rocket: Rocket, rocket_option, motor_kind
+        cls, flight_id: str, *, rocket: Rocket
     ) -> Union[FlightUpdated, HTTPException]:
         """
         Update a models.Flight.rocket in the database.
@@ -340,16 +284,16 @@ async def update_rocket_by_flight_id(
         try:
             read_flight = await cls.get_flight_by_id(flight_id)
             updated_rocket = rocket.dict()
-            updated_rocket["rocket_option"] = rocket_option
-            updated_rocket["motor"]["motor_kind"] = motor_kind
+            updated_rocket["rocket_option"] = rocket.rocket_option.value
+            updated_rocket["motor"][
+                "motor_kind"
+            ] = rocket.motor.motor_kind.value
             new_flight = read_flight.dict()
             new_flight["rocket"] = updated_rocket
             new_flight = Flight(**new_flight)
             async with FlightRepository() as flight_repo:
                 flight_repo.fetch_flight(new_flight)
-                await flight_repo.create_flight(
-                    motor_kind=motor_kind, rocket_option=rocket_option
-                )
+                await flight_repo.create_flight()
                 await flight_repo.delete_flight_by_id(flight_id)
         except PyMongoError as e:
             logger.error(
@@ -435,257 +379,8 @@ async def simulate_flight(
         """
         try:
             read_flight = await cls.get_flight_by_id(flight_id=flight_id)
-            flight = cls.get_rocketpy_flight(read_flight)
-
-            _initial_conditions = InitialConditions(
-                initial_altitude="Attitude - e0: {:.3f} | e1: {:.3f} | e2: {:.3f} | e3: {:.3f}".format(
-                    flight.e0(0), flight.e1(0), flight.e2(0), flight.e3(0)
-                ),
-                initial_velocity="Velocity - Vx: {:.2f} m/s | Vy: {:.2f} m/s | Vz: {:.2f} m/s".format(
-                    flight.vx(0), flight.vy(0), flight.vz(0)
-                ),
-                initial_position="Position - x: {:.2f} m | y: {:.2f} m | z: {:.2f} m".format(
-                    flight.x(0), flight.y(0), flight.z(0)
-                ),
-                initial_angular_position="Euler Angles - Spin φ : {:.2f}° | Nutation θ: {:.2f}° | Precession ψ: {:.2f}°".format(
-                    flight.phi(0), flight.theta(0), flight.psi(0)
-                ),
-                initial_angular_velocity="Angular Velocity - ω1: {:.2f} rad/s | ω2: {:.2f} rad/s| ω3: {:.2f} rad/s".format(
-                    flight.w1(0), flight.w2(0), flight.w3(0)
-                ),
-            )
-
-            _numerical_integration_settings = NumericalIntegrationSettings(
-                max_time="Maximum Allowed Flight Time: {:f} s".format(
-                    flight.max_time
-                ),
-                max_time_step="Maximum Allowed Time Step: {:f} s".format(
-                    flight.max_time_step
-                ),
-                min_time_step="Minimum Allowed Time Step: {:e} s".format(
-                    flight.min_time_step
-                ),
-                relative_error_tolerance=f"Relative Error Tolerance: {flight.rtol}",
-                absolute_error_tolerance=f"Absolute Error Tolerance: {flight.atol}",
-                time_overshoot=f"Allow Event Overshoot: {flight.time_overshoot}",
-                terminate_on_apogee=f"Terminate Simulation on Apogee: {flight.terminate_on_apogee}",
-                number_of_time_steps=f"Number of Time Steps Used: {len(flight.time_steps)}",
-                function_evaluations_per_time_step=f"Number of Derivative Functions Evaluation: {sum(flight.function_evaluations_per_time_step)}",
-                avg_function_evaluations_per_time_step="Average Function Evaluations per Time Step: {:3f}".format(
-                    sum(flight.function_evaluations_per_time_step)
-                    / len(flight.time_steps)
-                ),
-            )
-
-            _launch_rail_conditions = LaunchRailConditions(
-                rail_length="Launch Rail Length: {:.2f} m".format(
-                    flight.rail_length
-                ),
-                flight_inclination="Launch Rail Inclination: {:.2f}°".format(
-                    flight.inclination
-                ),
-                flight_heading="Launch Rail Heading: {:.2f}°".format(
-                    flight.heading
-                ),
-            )
-
-            _surface_wind_conditions = SurfaceWindConditions(
-                frontal_surface_wind_speed="Frontal Surface Wind Speed: {:.2f} m/s".format(
-                    flight.frontal_surface_wind
-                ),
-                lateral_surface_wind_speed="Lateral Surface Wind Speed: {:.2f} m/s".format(
-                    flight.lateral_surface_wind
-                ),
-            )
-
-            _out_of_rail_conditions = OutOfRailConditions(
-                out_of_rail_time="Rail Departure Time: {:.3f} s".format(
-                    flight.out_of_rail_time
-                ),
-                out_of_rail_velocity="Rail Departure Velocity: {:.3f} m/s".format(
-                    flight.out_of_rail_velocity
-                ),
-                out_of_rail_static_margin="Rail Departure Static Margin: {:.3f} c".format(
-                    flight.rocket.static_margin(flight.out_of_rail_time)
-                ),
-                out_of_rail_angle_of_attack="Rail Departure Angle of Attack: {:.3f}°".format(
-                    flight.angle_of_attack(flight.out_of_rail_time)
-                ),
-                out_of_rail_thrust_weight_ratio="Rail Departure Thrust-Weight Ratio: {:.3f}".format(
-                    flight.rocket.thrust_to_weight(flight.out_of_rail_time)
-                ),
-                out_of_rail_reynolds_number="Rail Departure Reynolds Number: {:.3e}".format(
-                    flight.reynolds_number(flight.out_of_rail_time)
-                ),
-            )
-
-            _burnout_conditions = BurnoutConditions(
-                burnout_time="Burn out time: {:.3f} s".format(
-                    flight.rocket.motor.burn_out_time
-                ),
-                burnout_altitude="Altitude at burn out: {:.3f} m (AGL)".format(
-                    flight.z(flight.rocket.motor.burn_out_time)
-                    - flight.env.elevation
-                ),
-                burnout_rocket_velocity="Rocket velocity at burn out: {:.3f} m/s".format(
-                    flight.speed(flight.rocket.motor.burn_out_time)
-                ),
-                burnout_freestream_velocity="Freestream velocity at burn out: {:.3f} m/s".format(
-                    (
-                        flight.stream_velocity_x(
-                            flight.rocket.motor.burn_out_time
-                        )
-                        ** 2
-                        + flight.stream_velocity_y(
-                            flight.rocket.motor.burn_out_time
-                        )
-                        ** 2
-                        + flight.stream_velocity_z(
-                            flight.rocket.motor.burn_out_time
-                        )
-                        ** 2
-                    )
-                    ** 0.5
-                ),
-                burnout_mach_number="Mach Number at burn out: {:.3f}".format(
-                    flight.mach_number(flight.rocket.motor.burn_out_time)
-                ),
-                burnout_kinetic_energy="Kinetic energy at burn out: {:.3e}".format(
-                    flight.kinetic_energy(flight.rocket.motor.burn_out_time)
-                ),
-            )
-
-            _apogee_conditions = ApogeeConditions(
-                apogee_altitude="Apogee Altitude: {:.3f} m (ASL) | {:.3f} m (AGL)".format(
-                    flight.apogee, flight.apogee - flight.env.elevation
-                ),
-                apogee_time="Apogee Time: {:.3f} s".format(flight.apogee_time),
-                apogee_freestream_speed="Apogee Freestream Speed: {:.3f} m/s".format(
-                    flight.apogee_freestream_speed
-                ),
-            )
-
-            _maximum_values = MaximumValues(
-                maximum_speed="Maximum Speed: {:.3f} m/s at {:.2f} s".format(
-                    flight.max_speed, flight.max_speed_time
-                ),
-                maximum_mach_number="Maximum Mach Number: {:.3f} Mach at {:.2f} s".format(
-                    flight.max_mach_number, flight.max_mach_number_time
-                ),
-                maximum_reynolds_number="Maximum Reynolds Number: {:.3e} at {:.2f} s".format(
-                    flight.max_reynolds_number, flight.max_reynolds_number_time
-                ),
-                maximum_dynamic_pressure="Maximum Dynamic Pressure: {:.3e} Pa at {:.2f} s".format(
-                    flight.max_dynamic_pressure,
-                    flight.max_dynamic_pressure_time,
-                ),
-                maximum_acceleration_during_motor_burn="Maximum Acceleration During Motor Burn: {:.3f} m/s² at {:.2f} s".format(
-                    flight.max_acceleration, flight.max_acceleration_time
-                ),
-                maximum_gs_during_motor_burn="Maximum Gs During Motor Burn: {:.3f} g at {:.2f} s".format(
-                    flight.max_acceleration
-                    / flight.env.gravity(
-                        flight.z(flight.max_acceleration_time)
-                    ),
-                    flight.max_acceleration_time,
-                ),
-                maximum_acceleration_after_motor_burn="Maximum Acceleration After Motor Burn: {:.3f} m/s² at {:.2f} s".format(
-                    flight.max_acceleration_power_off,
-                    flight.max_acceleration_power_off_time,
-                ),
-                maximum_gs_after_motor_burn="Maximum Gs After Motor Burn: {:.3f} g at {:.2f} s".format(
-                    flight.max_acceleration_power_off / flight.env.standard_g,
-                    flight.max_acceleration_power_off_time,
-                ),
-                maximum_upper_rail_button_normal_force="Maximum Upper Rail Button Normal Force: {:.3f} N".format(
-                    flight.max_rail_button1_normal_force
-                ),
-                maximum_upper_rail_button_shear_force="Maximum Upper Rail Button Shear Force: {:.3f} N".format(
-                    flight.max_rail_button1_shear_force
-                ),
-                maximum_lower_rail_button_normal_force="Maximum Lower Rail Button Normal Force: {:.3f} N".format(
-                    flight.max_rail_button2_normal_force
-                ),
-                maximum_lower_rail_button_shear_force="Maximum Lower Rail Button Shear Force: {:.3f} N".format(
-                    flight.max_rail_button2_shear_force
-                ),
-            )
-
-            if len(flight.impact_state) != 0:
-                _impact_conditions = ImpactConditions(
-                    x_impact_position="X Impact: {:.3f} m".format(
-                        flight.x_impact
-                    ),
-                    y_impact_position="Y Impact: {:.3f} m".format(
-                        flight.y_impact
-                    ),
-                    time_of_impact="Time of Impact: {:.3f} s".format(
-                        flight.t_final
-                    ),
-                    impact_velocity="Velocity at Impact: {:.3f} m/s".format(
-                        flight.impact_velocity
-                    ),
-                )
-            elif flight.terminate_on_apogee is False:
-                _impact_conditions = ImpactConditions(
-                    time="Time: {:.3f} s".format(flight.solution[-1][0]),
-                    altitude="Altitude: {:.3f} m".format(
-                        flight.solution[-1][3]
-                    ),
-                )
-
-            if len(flight.parachute_events) == 0:
-                _events_registered = EventsRegistered(
-                    events_trace="No parachute event registered"
-                )
-            else:
-                events = {}
-                for event in flight.parachute_events:
-                    trigger_time = event[0]
-                    parachute = event[1]
-                    open_time = trigger_time + parachute.lag
-                    velocity = flight.free_stream_speed(open_time)
-                    altitude = flight.z(open_time)
-                    name = parachute.name.title()
-                    events[name] = []
-                    events[name].append(
-                        name
-                        + " Ejection Triggered at: {:.3f} s".format(
-                            trigger_time
-                        )
-                    )
-                    events[name].append(
-                        name
-                        + " Parachute Inflated at: {:.3f} s".format(open_time)
-                    )
-                    events[name].append(
-                        name
-                        + " Parachute Inflated with Freestream Speed of: {:.3f} m/s".format(
-                            velocity
-                        )
-                    )
-                    events[name].append(
-                        name
-                        + " Parachute Inflated at Height of: {:.3f} m (AGL)".format(
-                            altitude - flight.env.elevation
-                        )
-                    )
-                _events_registered = EventsRegistered(events_trace=events)
-
-            _flight_data = FlightData(
-                initial_conditions=_initial_conditions,
-                numerical_integration_settings=_numerical_integration_settings,
-                surface_wind_conditions=_surface_wind_conditions,
-                launch_rail_conditions=_launch_rail_conditions,
-                out_of_rail_conditions=_out_of_rail_conditions,
-                burnout_conditions=_burnout_conditions,
-                apogee_conditions=_apogee_conditions,
-                maximum_values=_maximum_values,
-                impact_conditions=_impact_conditions,
-                events_registered=_events_registered,
-            )
-
-            flight_summary = FlightSummary(flight_data=_flight_data)
+            rocketpy_flight = FlightService.from_flight_model(read_flight)
+            flight_summary = rocketpy_flight.get_flight_summary()
         except HTTPException as e:
             raise e from e
         except Exception as e:
diff --git a/lib/controllers/motor.py b/lib/controllers/motor.py
index 2ba8588..3d98eb1 100644
--- a/lib/controllers/motor.py
+++ b/lib/controllers/motor.py
@@ -1,17 +1,14 @@
 from typing import Union
 from fastapi import HTTPException, status
 from pymongo.errors import PyMongoError
-from rocketpy.motors.solid_motor import SolidMotor
-from rocketpy.motors.liquid_motor import LiquidMotor
-from rocketpy.motors.hybrid_motor import HybridMotor
 import jsonpickle
 
 from lib import logger, parse_error
 from lib.models.motor import Motor, MotorKinds
+from lib.services.motor import MotorService
 from lib.repositories.motor import MotorRepository
 from lib.views.motor import (
     MotorSummary,
-    MotorData,
     MotorCreated,
     MotorUpdated,
     MotorDeleted,
@@ -30,10 +27,9 @@ class MotorController:
         - Create a rocketpy.Motor object from a Motor model object.
     """
 
-    def __init__(self, *, motor: Motor, motor_kind: MotorKinds):
-        self.guard(motor, motor_kind)
+    def __init__(self, motor: Motor):
+        self.guard(motor)
         self._motor = motor
-        self._motor_kind = motor_kind
 
     @property
     def motor(self) -> Motor:
@@ -43,67 +39,8 @@ def motor(self) -> Motor:
     def motor(self, motor: Motor):
         self._motor = motor
 
-    @property
-    def motor_kind(self) -> MotorKinds:
-        return self._motor_kind
-
-    @staticmethod
-    def get_rocketpy_motor(
-        motor: Motor,
-    ) -> Union[LiquidMotor, HybridMotor, SolidMotor]:
-        """
-        Get the rocketpy motor object.
-
-        Returns:
-            Union[LiquidMotor, HybridMotor, SolidMotor]
-        """
-
-        motor_core = {
-            "thrust_source": f"lib/data/engines/{motor.thrust_source.value}.eng",
-            "burn_time": motor.burn_time,
-            "nozzle_radius": motor.nozzle_radius,
-            "dry_mass": motor.dry_mass,
-            "dry_inertia": motor.dry_inertia,
-            "center_of_dry_mass_position": motor.center_of_dry_mass_position,
-        }
-
-        match motor.motor_kind:
-            case MotorKinds.LIQUID:
-                rocketpy_motor = LiquidMotor(**motor_core)
-            case MotorKinds.HYBRID:
-                rocketpy_motor = HybridMotor(
-                    **motor_core,
-                    throat_radius=motor.throat_radius,
-                    grain_number=motor.grain_number,
-                    grain_density=motor.grain_density,
-                    grain_outer_radius=motor.grain_outer_radius,
-                    grain_initial_inner_radius=motor.grain_initial_inner_radius,
-                    grain_initial_height=motor.grain_initial_height,
-                    grain_separation=motor.grain_separation,
-                    grains_center_of_mass_position=motor.grains_center_of_mass_position,
-                )
-            case _:
-                rocketpy_motor = SolidMotor(
-                    **motor_core,
-                    grain_number=motor.grain_number,
-                    grain_density=motor.grain_density,
-                    grain_outer_radius=motor.grain_outer_radius,
-                    grain_initial_inner_radius=motor.grain_initial_inner_radius,
-                    grain_initial_height=motor.grain_initial_height,
-                    grains_center_of_mass_position=motor.grains_center_of_mass_position,
-                    grain_separation=motor.grain_separation,
-                    throat_radius=motor.throat_radius,
-                    interpolation_method=motor.interpolation_method,
-                )
-
-        if motor.motor_kind != MotorKinds.SOLID:
-            for tank in motor.tanks:
-                rocketpy_motor.add_tank(tank.tank, tank.position)
-
-        return rocketpy_motor
-
-    def guard(self, motor: Motor, motor_kind):
-        if motor_kind != MotorKinds.SOLID and motor.tanks is None:
+    def guard(self, motor: Motor):
+        if motor.motor_kind != MotorKinds.SOLID and motor.tanks is None:
             raise HTTPException(
                 status_code=status.HTTP_422_UNPROCESSABLE_ENTITY,
                 detail="Tanks must be provided for liquid and hybrid motors.",
@@ -119,7 +56,7 @@ async def create_motor(self) -> Union[MotorCreated, HTTPException]:
         try:
             async with MotorRepository() as motor_repo:
                 motor_repo.fetch_motor(self.motor)
-                await motor_repo.create_motor(motor_kind=self.motor_kind)
+                await motor_repo.create_motor()
         except PyMongoError as e:
             logger.error(f"controllers.motor.create_motor: PyMongoError {e}")
             raise HTTPException(
@@ -208,7 +145,7 @@ async def get_rocketpy_motor_as_jsonpickle(
         """
         try:
             read_motor = await cls.get_motor_by_id(motor_id)
-            rocketpy_motor = cls.get_rocketpy_motor(read_motor)
+            rocketpy_motor = MotorService.from_motor_model(read_motor)
         except HTTPException as e:
             raise e from e
         except Exception as e:
@@ -247,7 +184,7 @@ async def update_motor_by_id(
         try:
             async with MotorRepository() as motor_repo:
                 motor_repo.fetch_motor(self.motor)
-                await motor_repo.create_motor(motor_kind=self.motor_kind)
+                await motor_repo.create_motor()
                 await motor_repo.delete_motor_by_id(motor_id)
         except PyMongoError as e:
             logger.error(f"controllers.motor.update_motor: PyMongoError {e}")
@@ -330,38 +267,8 @@ async def simulate_motor(
         """
         try:
             read_motor = await cls.get_motor_by_id(motor_id)
-            motor = cls.get_rocketpy_motor(read_motor)
-
-            motor_simulation_numbers = MotorData(
-                total_burning_time="Total Burning Time: "
-                + str(motor.burn_out_time)
-                + " s",
-                total_propellant_mass="Total Propellant Mass: "
-                + "{:.3f}".format(motor.propellant_initial_mass)
-                + " kg",
-                average_propellant_exhaust_velocity="Average Propellant Exhaust Velocity: "
-                + "{:.3f}".format(
-                    motor.exhaust_velocity.average(*motor.burn_time)
-                )
-                + " m/s",
-                average_thrust="Average Thrust: "
-                + "{:.3f}".format(motor.average_thrust)
-                + " N",
-                maximum_thrust="Maximum Thrust: "
-                + str(motor.max_thrust)
-                + " N at "
-                + str(motor.max_thrust_time)
-                + " s after ignition.",
-                total_impulse="Total Impulse: "
-                + "{:.3f}".format(motor.total_impulse)
-                + " Ns\n",
-            )
-            # motor_simulation_plots = MotorPlots(
-            #    motor.thrust.plot(lower=lower_limit, upper=upper_limit)
-            # )
-            motor_summary = MotorSummary(
-                motor_data=motor_simulation_numbers
-            )  # , plots=motor_simulation_plots )
+            rocketpy_motor = MotorService.from_motor_model(read_motor)
+            motor_summary = rocketpy_motor.get_motor_summary()
         except HTTPException as e:
             raise e from e
         except Exception as e:
diff --git a/lib/controllers/rocket.py b/lib/controllers/rocket.py
index 90b54a3..968d1b1 100644
--- a/lib/controllers/rocket.py
+++ b/lib/controllers/rocket.py
@@ -1,6 +1,4 @@
 from typing import Union
-import os
-import ast
 import jsonpickle
 
 from fastapi import HTTPException, status
@@ -9,27 +7,11 @@
 # TODO
 # from inspect import getsourcelines
 
-from rocketpy.rocket.parachute import Parachute as RocketPyParachute
-from rocketpy.rocket.rocket import Rocket as RocketPyRocket
-from rocketpy.rocket.aero_surface import NoseCone as RocketPyNoseCone
-from rocketpy.rocket.aero_surface import (
-    TrapezoidalFins as RocketPyTrapezoidalFins,
-)
-from rocketpy.rocket.aero_surface import Tail as RocketPyTail
-
 from lib import logger, parse_error
-from lib.controllers.motor import MotorController
-from lib.models.rocket import Rocket, RocketOptions
-from lib.models.motor import MotorKinds
-from lib.models.aerosurfaces import NoseCone, TrapezoidalFins, Tail
-from lib.models.parachute import Parachute
+from lib.services.rocket import RocketService
+from lib.models.rocket import Rocket
 from lib.repositories.rocket import RocketRepository
 from lib.views.rocket import (
-    InertiaDetails,
-    RocketGeometricalParameters,
-    RocketAerodynamicsQuantities,
-    ParachuteData,
-    RocketData,
     RocketSummary,
     RocketCreated,
     RocketUpdated,
@@ -51,14 +33,9 @@ class RocketController:
 
     def __init__(
         self,
-        *,
         rocket: Rocket,
-        rocket_option: RocketOptions,
-        motor_kind: MotorKinds,
     ):
         self._rocket = rocket
-        self._rocket_option = rocket_option
-        self._motor_kind = motor_kind
 
     @property
     def rocket(self) -> Rocket:
@@ -68,84 +45,6 @@ def rocket(self) -> Rocket:
     def rocket(self, rocket: Rocket):
         self._rocket = rocket
 
-    @property
-    def rocket_option(self) -> RocketOptions:
-        return self._rocket_option
-
-    @property
-    def motor_kind(self) -> MotorKinds:
-        return self._motor_kind
-
-    @classmethod
-    def get_rocketpy_rocket(cls, rocket: Rocket) -> RocketPyRocket:
-        """
-        Get a rocketpy rocket object.
-
-        Returns:
-            RocketPyRocket
-        """
-
-        rocketpy_rocket = RocketPyRocket(
-            radius=rocket.radius,
-            mass=rocket.mass,
-            inertia=rocket.inertia,
-            power_off_drag=os.path.join(
-                "lib/data",
-                f"{rocket.rocket_option.lower()}",
-                "powerOffDragCurve.csv",
-            ),
-            power_on_drag=os.path.join(
-                "lib/data",
-                f"{rocket.rocket_option.lower()}",
-                "powerOnDragCurve.csv",
-            ),
-            center_of_mass_without_motor=rocket.center_of_mass_without_motor,
-            coordinate_system_orientation=rocket.coordinate_system_orientation,
-        )
-
-        # RailButtons
-        rocketpy_rocket.set_rail_buttons(
-            upper_button_position=rocket.rail_buttons.upper_button_position,
-            lower_button_position=rocket.rail_buttons.lower_button_position,
-            angular_position=rocket.rail_buttons.angular_position,
-        )
-        rocketpy_rocket.add_motor(
-            MotorController.get_rocketpy_motor(rocket.motor),
-            rocket.motor_position,
-        )
-
-        # NoseCone
-        nose = cls.get_rocketpy_nose(rocket.nose)
-        rocketpy_rocket.aerodynamic_surfaces.add(nose, nose.position)
-        rocketpy_rocket.evaluate_static_margin()
-
-        # FinSet
-        # TODO: re-write this to match overall fins not only TrapezoidalFins
-        # Maybe a strategy with different factory methods?
-        finset = cls.get_rocketpy_finset(rocket.fins)
-        rocketpy_rocket.aerodynamic_surfaces.add(finset, finset.position)
-        rocketpy_rocket.evaluate_static_margin()
-
-        # Tail
-        tail = cls.get_rocketpy_tail(rocket.tail)
-        rocketpy_rocket.aerodynamic_surfaces.add(tail, tail.position)
-        rocketpy_rocket.evaluate_static_margin()
-
-        # Parachutes
-        for p in range(len(rocket.parachutes)):
-            parachute_trigger = rocket.parachutes[p].triggers[0]
-            if cls.check_parachute_trigger(parachute_trigger):
-                rocket.parachutes[p].triggers[0] = compile(
-                    parachute_trigger, "<string>", "eval"
-                )
-                parachute = cls.get_rocketpy_parachute(rocket.parachutes, p)
-                rocketpy_rocket.parachutes.append(parachute)
-            else:
-                print("Parachute trigger not valid. Skipping parachute.")
-                continue
-
-        return rocketpy_rocket
-
     async def create_rocket(self) -> Union[RocketCreated, HTTPException]:
         """
         Create a models.Rocket in the database.
@@ -156,10 +55,7 @@ async def create_rocket(self) -> Union[RocketCreated, HTTPException]:
         try:
             async with RocketRepository() as rocket_repo:
                 rocket_repo.fetch_rocket(self.rocket)
-                await rocket_repo.create_rocket(
-                    rocket_option=self.rocket_option,
-                    motor_kind=self.motor_kind,
-                )
+                await rocket_repo.create_rocket()
         except PyMongoError as e:
             logger.error(f"controllers.rocket.create_rocket: PyMongoError {e}")
             raise HTTPException(
@@ -249,7 +145,7 @@ async def get_rocketpy_rocket_as_jsonpickle(
         """
         try:
             read_rocket = await cls.get_rocket_by_id(rocket_id)
-            rocketpy_rocket = cls.get_rocketpy_rocket(read_rocket)
+            rocketpy_rocket = RocketService.from_rocket_model(read_rocket)
         except HTTPException as e:
             raise e from e
         except Exception as e:
@@ -288,10 +184,7 @@ async def update_rocket_by_id(
         try:
             async with RocketRepository() as rocket_repo:
                 rocket_repo.fetch_rocket(self.rocket)
-                await rocket_repo.create_rocket(
-                    rocket_option=self.rocket_option,
-                    motor_kind=self.motor_kind,
-                )
+                await rocket_repo.create_rocket()
                 await rocket_repo.delete_rocket_by_id(rocket_id)
         except PyMongoError as e:
             logger.error(f"controllers.rocket.update_rocket: PyMongoError {e}")
@@ -375,146 +268,8 @@ async def simulate_rocket(
         """
         try:
             read_rocket = await cls.get_rocket_by_id(rocket_id)
-            rocket = cls.get_rocketpy_rocket(read_rocket)
-
-            _inertia_details = InertiaDetails(
-                rocket_mass_without_propellant="Rocket Mass: {:.3f} kg (No Propellant)".format(
-                    rocket.mass
-                ),
-                rocket_mass_with_propellant="Rocket Mass: {:.3f} kg (With Propellant)".format(
-                    rocket.total_mass(0)
-                ),
-                rocket_inertia_with_motor_without_propellant=[
-                    "Rocket Inertia (with motor, but without propellant) 11: {:.3f} kg*m2".format(
-                        rocket.dry_I_11
-                    ),
-                    "Rocket Inertia (with motor, but without propellant) 22: {:.3f} kg*m2".format(
-                        rocket.dry_I_22
-                    ),
-                    "Rocket Inertia (with motor, but without propellant) 33: {:.3f} kg*m2".format(
-                        rocket.dry_I_33
-                    ),
-                    "Rocket Inertia (with motor, but without propellant) 12: {:.3f} kg*m2".format(
-                        rocket.dry_I_12
-                    ),
-                    "Rocket Inertia (with motor, but without propellant) 13: {:.3f} kg*m2".format(
-                        rocket.dry_I_13
-                    ),
-                    "Rocket Inertia (with motor, but without propellant) 23: {:.3f} kg*m2".format(
-                        rocket.dry_I_23
-                    ),
-                ],
-            )
-
-            _rocket_geometrical_parameters = RocketGeometricalParameters(
-                rocket_maximum_radius="Rocket Maximum Radius: "
-                + str(rocket.radius)
-                + " m",
-                rocket_frontal_area="Rocket Frontal Area: "
-                + "{:.6f}".format(rocket.area)
-                + " m2",
-                rocket_codm_nozzle_exit_distance="Rocket Center of Dry Mass - Nozzle Exit Distance: "
-                + "{:.3f} m".format(
-                    abs(
-                        rocket.center_of_dry_mass_position
-                        - rocket.motor_position
-                    )
-                ),
-                rocket_codm_center_of_propellant_mass="Rocket Center of Dry Mass - Center of Propellant Mass: "
-                + "{:.3f} m".format(
-                    abs(
-                        rocket.center_of_propellant_position(0)
-                        - rocket.center_of_dry_mass_position
-                    )
-                ),
-                rocket_codm_loaded_center_of_mass="Rocket Center of Mass - Rocket Loaded Center of Mass: "
-                + "{:.3f} m".format(
-                    abs(
-                        rocket.center_of_mass(0)
-                        - rocket.center_of_dry_mass_position
-                    )
-                ),
-            )
-
-            _aerodynamics_lift_coefficient_derivatives = {}
-            for surface, _position in rocket.aerodynamic_surfaces:
-                name = surface.name
-                _aerodynamics_lift_coefficient_derivatives[name] = []
-                _aerodynamics_lift_coefficient_derivatives[name].append(
-                    name
-                    + " Lift Coefficient Derivative: {:.3f}".format(
-                        surface.clalpha(0)
-                    )
-                    + "/rad"
-                )
-
-            _aerodynamics_center_of_pressure = {}
-            for surface, _position in rocket.aerodynamic_surfaces:
-                name = surface.name
-                cpz = surface.cp[2]
-                _aerodynamics_center_of_pressure[name] = []
-                _aerodynamics_center_of_pressure[name].append(
-                    name
-                    + " Center of Pressure to CM: {:.3f}".format(cpz)
-                    + " m"
-                )
-
-            _rocket_aerodynamics_quantities = RocketAerodynamicsQuantities(
-                aerodynamics_lift_coefficient_derivatives=_aerodynamics_lift_coefficient_derivatives,
-                aerodynamics_center_of_pressure=_aerodynamics_center_of_pressure,
-                distance_cop_to_codm="Distance from Center of Pressure to Center of Dry Mass: "
-                + "{:.3f}".format(
-                    rocket.center_of_mass(0) - rocket.cp_position(0)
-                )
-                + " m",
-                initial_static_margin="Initial Static Margin: "
-                + "{:.3f}".format(rocket.static_margin(0))
-                + " c",
-                final_static_margin="Final Static Margin: "
-                + "{:.3f}".format(
-                    rocket.static_margin(rocket.motor.burn_out_time)
-                )
-                + " c",
-            )
-
-            _parachute_details = {}
-            _parachute_ejection_signal_trigger = {}
-            _parachute_ejection_system_refresh_rate = {}
-            _parachute_lag = {}
-            for chute in rocket.parachutes:
-                _parachute_details[chute.name] = chute.__str__()
-
-                if chute.trigger.__name__ == "<lambda>":
-                    # line = getsourcelines(chute.trigger)[0][0]
-                    # _parachute_ejection_signal_trigger[chute.name] = "Ejection signal trigger: " + line.split("lambda ")[1].split(",")[0].split("\n")[0]
-                    pass
-
-                else:
-                    _parachute_ejection_signal_trigger[chute.name] = (
-                        "Ejection signal trigger: " + chute.trigger.__name__
-                    )
-                    _parachute_ejection_system_refresh_rate[chute.name] = (
-                        "Ejection system refresh rate: {chute.sampling_rate:.3f} Hz"
-                    )
-                    _parachute_lag[chute.name] = (
-                        "Time between ejection signal is triggered and the parachute is fully opened: {chute.lag:.1f} s\n"
-                    )
-
-            _parachute_data = ParachuteData(
-                parachute_details=_parachute_details,
-                # parachute_ejection_signal_trigger = _parachute_ejection_signal_trigger,
-                parachute_ejection_system_refresh_rate=_parachute_ejection_system_refresh_rate,
-                parachute_lag=_parachute_lag,
-            )
-
-            _rocket_data = RocketData(
-                inertia_details=_inertia_details,
-                rocket_geometrical_parameters=_rocket_geometrical_parameters,
-                rocket_aerodynamics_quantities=_rocket_aerodynamics_quantities,
-                parachute_data=_parachute_data,
-            )
-
-            rocket_summary = RocketSummary(rocket_data=_rocket_data)
+            rocketpy_rocket = RocketService.from_rocket_model(read_rocket)
+            rocket_summary = rocketpy_rocket.get_rocket_summary()
         except HTTPException as e:
             raise e from e
         except Exception as e:
@@ -530,141 +285,3 @@ async def simulate_rocket(
             logger.info(
                 f"Call to controllers.rocket.simulate completed for Rocket {rocket_id}"
             )
-
-    @staticmethod
-    def get_rocketpy_nose(nose: NoseCone) -> RocketPyNoseCone:
-        """
-        Get a rocketpy nose cone object.
-
-        Returns:
-            RocketPyNoseCone
-        """
-
-        rocketpy_nose = RocketPyNoseCone(
-            length=nose.length,
-            kind=nose.kind,
-            base_radius=nose.base_radius,
-            rocket_radius=nose.rocket_radius,
-        )
-        rocketpy_nose.position = nose.position
-        return rocketpy_nose
-
-    @staticmethod
-    def get_rocketpy_finset(
-        trapezoidal_fins: TrapezoidalFins,
-    ) -> RocketPyTrapezoidalFins:
-        """
-        Get a rocketpy finset object.
-
-        Returns:
-            RocketPyTrapezoidalFins
-        """
-        rocketpy_finset = RocketPyTrapezoidalFins(
-            n=trapezoidal_fins.n,
-            root_chord=trapezoidal_fins.root_chord,
-            tip_chord=trapezoidal_fins.tip_chord,
-            span=trapezoidal_fins.span,
-            cant_angle=trapezoidal_fins.cant_angle,
-            rocket_radius=trapezoidal_fins.radius,
-            airfoil=trapezoidal_fins.airfoil,
-        )
-        rocketpy_finset.position = trapezoidal_fins.position
-        return rocketpy_finset
-
-    @staticmethod
-    def get_rocketpy_tail(tail: Tail) -> RocketPyTail:
-        """
-        Get a rocketpy tail object.
-
-        Returns:
-            RocketPyTail
-        """
-        rocketpy_tail = RocketPyTail(
-            top_radius=tail.top_radius,
-            bottom_radius=tail.bottom_radius,
-            length=tail.length,
-            rocket_radius=tail.radius,
-        )
-        rocketpy_tail.position = tail.position
-        return rocketpy_tail
-
-    @staticmethod
-    def get_rocketpy_parachute(
-        parachute: Parachute, p: int
-    ) -> RocketPyParachute:
-        """
-        Get a rocketpy parachute object.
-
-        Returns:
-            RocketPyParachute
-        """
-        rocketpy_parachute = RocketPyParachute(
-            name=parachute[p].name[0],
-            cd_s=parachute[p].cd_s[0],
-            trigger=eval(parachute[p].triggers[0]),
-            sampling_rate=parachute[p].sampling_rate[0],
-            lag=parachute[p].lag[0],
-            noise=parachute[p].noise[0],
-        )
-        return rocketpy_parachute
-
-    @staticmethod
-    def check_parachute_trigger(expression: str) -> bool:
-        """
-        Check if the trigger expression is valid.
-
-        Args:
-            expression: str
-
-        Returns:
-            bool: True if the expression is valid, False otherwise.
-        """
-
-        # Parsing the expression into an AST
-        try:
-            parsed_expression = ast.parse(expression, mode="eval")
-        except SyntaxError:
-            print("Invalid syntax.")
-            return False
-
-        # Constant case (supported after beta v1)
-        if isinstance(parsed_expression.body, ast.Constant):
-            return True
-        # Name case (supported after beta v1)
-        if (
-            isinstance(parsed_expression.body, ast.Name)
-            and parsed_expression.body.id == "apogee"
-        ):
-            global apogee
-            apogee = "apogee"
-            return True
-
-        # Validating the expression structure
-        if not isinstance(parsed_expression.body, ast.Lambda):
-            print("Invalid expression structure (not a Lambda).")
-            return False
-
-        lambda_node = parsed_expression.body
-        if len(lambda_node.args.args) != 3:
-            print("Invalid expression structure (invalid arity).")
-            return False
-
-        if not isinstance(lambda_node.body, ast.Compare):
-            try:
-                for operand in lambda_node.body.values:
-                    if not isinstance(operand, ast.Compare):
-                        print("Invalid expression structure (not a Compare).")
-                        return False
-            except AttributeError:
-                print("Invalid expression structure (not a Compare).")
-                return False
-
-        # Restricting access to functions or attributes
-        for node in ast.walk(lambda_node):
-            if isinstance(node, ast.Call):
-                print("Calling functions is not allowed in the expression.")
-                return False
-            if isinstance(node, ast.Attribute):
-                print("Accessing attributes is not allowed in the expression.")
-                return False
-        return True
diff --git a/lib/models/motor.py b/lib/models/motor.py
index 1598b49..98d60fa 100644
--- a/lib/models/motor.py
+++ b/lib/models/motor.py
@@ -128,14 +128,14 @@ class Motor(BaseModel, frozen=True):
         "nozzle_to_combustion_chamber"
     )
 
-    def __init__(self, motor_kind=MotorKinds.SOLID, **kwargs):
-        super().__init__(**kwargs)
-        self._motor_kind = motor_kind
-
     @property
     def motor_kind(self) -> MotorKinds:
         return self._motor_kind
 
+    @motor_kind.setter
+    def motor_kind(self, motor_kind: MotorKinds):
+        self._motor_kind = motor_kind
+
     @property
     def motor_id(self) -> str:
         return str(hash(self))
diff --git a/lib/models/rocket.py b/lib/models/rocket.py
index b78e1b6..522e28e 100644
--- a/lib/models/rocket.py
+++ b/lib/models/rocket.py
@@ -40,10 +40,6 @@ class Rocket(BaseModel, frozen=True):
     # TODO: implement field validation so a list of possible tailToNose values is provided in the api docs
     coordinate_system_orientation: Optional[str] = "tail_to_nose"
 
-    def __init__(self, rocket_option=RocketOptions.CALISTO, **kwargs):
-        super().__init__(**kwargs)
-        self._rocket_option = rocket_option
-
     @property
     def rocket_option(self) -> RocketOptions:
         return self._rocket_option
diff --git a/lib/repositories/flight.py b/lib/repositories/flight.py
index ac68549..8b3d3ab 100644
--- a/lib/repositories/flight.py
+++ b/lib/repositories/flight.py
@@ -54,24 +54,22 @@ async def delete_flight(self, flight_id: str):
         await collection.delete_one({"flight_id": flight_id})
         return self
 
-    async def create_flight(
-        self, *, motor_kind: str = "SOLID", rocket_option: str = "CALISTO"
-    ):
+    async def create_flight(self):
         """
         Creates a non-existing models.Flight in the database
 
-        Args:
-            rocket_option: models.rocket.RocketOptions
-            motor_kind: models.motor.MotorKinds
-
         Returns:
             self
         """
         try:
             flight_to_dict = self.flight.dict()
             flight_to_dict["flight_id"] = self.flight_id
-            flight_to_dict["rocket"]["rocket_option"] = rocket_option
-            flight_to_dict["rocket"]["motor"]["motor_kind"] = motor_kind
+            flight_to_dict["rocket"][
+                "rocket_option"
+            ] = self.flight.rocket.rocket_option.value
+            flight_to_dict["rocket"]["motor"][
+                "motor_kind"
+            ] = self.flight.rocket.motor.motor_kind.value
             await self.insert_flight(flight_to_dict)
         except PyMongoError as e:
             raise e from e
diff --git a/lib/repositories/motor.py b/lib/repositories/motor.py
index 806016a..2395953 100644
--- a/lib/repositories/motor.py
+++ b/lib/repositories/motor.py
@@ -55,20 +55,17 @@ async def delete_motor(self, motor_id: str):
         await collection.delete_one({"motor_id": motor_id})
         return self
 
-    async def create_motor(self, motor_kind: str = "SOLID"):
+    async def create_motor(self):
         """
         Creates a non-existing models.Motor in the database
 
-        Args:
-            motor_kind: models.motor.MotorKinds
-
         Returns:
             self
         """
         try:
             motor_to_dict = self.motor.dict()
             motor_to_dict["motor_id"] = self.motor_id
-            motor_to_dict["motor_kind"] = motor_kind
+            motor_to_dict["motor_kind"] = motor.motor_kind.value
             await self.insert_motor(motor_to_dict)
         except PyMongoError as e:
             raise e from e
diff --git a/lib/repositories/repo.py b/lib/repositories/repo.py
index 4a56810..9a9f7ae 100644
--- a/lib/repositories/repo.py
+++ b/lib/repositories/repo.py
@@ -1,12 +1,18 @@
 import asyncio
 import threading
-from lib import logger
-from lib.secrets import Secrets
+
+from tenacity import (
+    stop_after_attempt,
+    wait_fixed,
+    retry,
+)
 from pydantic import BaseModel
-from fastapi import HTTPException, status
-from motor.motor_asyncio import AsyncIOMotorClient
 from pymongo.server_api import ServerApi
-from tenacity import retry, stop_after_attempt, wait_fixed
+from motor.motor_asyncio import AsyncIOMotorClient
+from fastapi import HTTPException, status
+
+from lib import logger
+from lib.secrets import Secrets
 
 
 class RepositoryNotInitializedException(HTTPException):
diff --git a/lib/repositories/rocket.py b/lib/repositories/rocket.py
index 2c74cee..e6a20d8 100644
--- a/lib/repositories/rocket.py
+++ b/lib/repositories/rocket.py
@@ -55,24 +55,20 @@ async def delete_rocket(self, rocket_id: str):
         await collection.delete_one({"rocket_id": rocket_id})
         return self
 
-    async def create_rocket(
-        self, *, rocket_option: str = "CALISTO", motor_kind: str = "SOLID"
-    ):
+    async def create_rocket(self):
         """
         Creates a non-existing models.Rocket in the database
 
-        Args:
-            rocket_option: models.rocket.RocketOptions
-            motor_kind: models.motor.MotorKinds
-
         Returns:
             self
         """
         try:
             rocket_to_dict = self.rocket.dict()
             rocket_to_dict["rocket_id"] = self.rocket_id
-            rocket_to_dict["rocket_option"] = rocket_option
-            rocket_to_dict["motor"]["motor_kind"] = motor_kind
+            rocket_to_dict["rocket_option"] = self.rocket.rocket_option.value
+            rocket_to_dict["motor"][
+                "motor_kind"
+            ] = self.rocket.motor.motor_kind.value
             await self.insert_rocket(rocket_to_dict)
         except PyMongoError as e:
             raise e from e
diff --git a/lib/routes/flight.py b/lib/routes/flight.py
index 2d597c6..4ea4a9b 100644
--- a/lib/routes/flight.py
+++ b/lib/routes/flight.py
@@ -42,9 +42,9 @@ async def create_flight(
     ``` Flight object as JSON ```
     """
     with tracer.start_as_current_span("create_flight"):
-        return await FlightController(
-            flight, rocket_option=rocket_option, motor_kind=motor_kind
-        ).create_flight()
+        flight.rocket.rocket_option = rocket_option
+        flight.rocket.motor.motor_kind = motor_kind
+        return await FlightController(flight).create_flight()
 
 
 @router.get("/{flight_id}")
@@ -107,11 +107,11 @@ async def update_flight_rocket(
     ```
     """
     with tracer.start_as_current_span("update_flight_rocket"):
+        rocket.rocket_option = rocket_option
+        rocket.motor.motor_kind = motor_kind
         return await FlightController.update_rocket_by_flight_id(
             flight_id,
             rocket=rocket,
-            rocket_option=rocket_option,
-            motor_kind=motor_kind,
         )
 
 
@@ -132,9 +132,9 @@ async def update_flight(
     ```
     """
     with tracer.start_as_current_span("update_flight"):
-        return await FlightController(
-            flight, rocket_option=rocket_option, motor_kind=motor_kind
-        ).update_flight_by_id(flight_id)
+        flight.rocket.rocket_option = rocket_option
+        flight.rocket.motor.motor_kind = motor_kind
+        return await FlightController(flight).update_flight_by_id(flight_id)
 
 
 @router.delete("/{flight_id}")
diff --git a/lib/routes/motor.py b/lib/routes/motor.py
index 5c4cbff..375e4fb 100644
--- a/lib/routes/motor.py
+++ b/lib/routes/motor.py
@@ -37,9 +37,8 @@ async def create_motor(motor: Motor, motor_kind: MotorKinds) -> MotorCreated:
     ``` Motor object as a JSON ```
     """
     with tracer.start_as_current_span("create_motor"):
-        return await MotorController(
-            motor=motor, motor_kind=motor_kind
-        ).create_motor()
+        motor.motor_kind = motor_kind
+        return await MotorController(motor).create_motor()
 
 
 @router.get("/{motor_id}")
@@ -68,9 +67,8 @@ async def update_motor(
     ```
     """
     with tracer.start_as_current_span("update_motor"):
-        return await MotorController(
-            motor=motor, motor_kind=motor_kind
-        ).update_motor_by_id(motor_id)
+        motor.motor_kind = motor_kind
+        return await MotorController(motor).update_motor_by_id(motor_id)
 
 
 @router.delete("/{motor_id}")
diff --git a/lib/routes/rocket.py b/lib/routes/rocket.py
index 1d7301e..e2faa91 100644
--- a/lib/routes/rocket.py
+++ b/lib/routes/rocket.py
@@ -40,9 +40,9 @@ async def create_rocket(
     ``` Rocket object as a JSON ```
     """
     with tracer.start_as_current_span("create_rocket"):
-        return await RocketController(
-            rocket=rocket, rocket_option=rocket_option, motor_kind=motor_kind
-        ).create_rocket()
+        rocket.rocket_option = rocket_option
+        rocket.motor.motor_kind = motor_kind
+        return await RocketController(rocket).create_rocket()
 
 
 @router.get("/{rocket_id}")
@@ -74,9 +74,9 @@ async def update_rocket(
     ```
     """
     with tracer.start_as_current_span("update_rocket"):
-        return await RocketController(
-            rocket=rocket, rocket_option=rocket_option, motor_kind=motor_kind
-        ).update_rocket_by_id(rocket_id)
+        rocket.rocket_option = rocket_option
+        rocket.motor.motor_kind = motor_kind
+        return await RocketController(rocket).update_rocket_by_id(rocket_id)
 
 
 @router.delete("/{rocket_id}")
diff --git a/lib/services/flight.py b/lib/services/flight.py
new file mode 100644
index 0000000..d8fcaca
--- /dev/null
+++ b/lib/services/flight.py
@@ -0,0 +1,291 @@
+from typing import Self
+
+from rocketpy.simulation.flight import Flight as RocketPyFlight
+from rocketpy.utilities import get_instance_attributes
+
+from lib.models.flight import Flight
+from lib.services.environment import EnvironmentService
+from lib.services.rocket import RocketService
+from lib.views.flight import (
+    FlightSummary,
+    SurfaceWindConditions,
+    OutOfRailConditions,
+    BurnoutConditions,
+    ApogeeConditions,
+    MaximumValues,
+    InitialConditions,
+    NumericalIntegrationSettings,
+    ImpactConditions,
+    EventsRegistered,
+    LaunchRailConditions,
+    FlightData,
+)
+
+
+class FlightService(RocketPyFlight):
+
+    @classmethod
+    def from_flight_model(cls, flight: Flight) -> Self:
+        """
+        Get the rocketpy flight object.
+
+        Returns:
+            RocketPyFlight
+        """
+        rocketpy_rocket = RocketService.from_rocket_model(flight.rocket)
+        rocketpy_env = EnvironmentService.from_env_model(flight.environment)
+        rocketpy_flight = RocketPyFlight(
+            rocket=rocketpy_rocket,
+            inclination=flight.inclination,
+            heading=flight.heading,
+            environment=rocketpy_env,
+            rail_length=flight.rail_length,
+        )
+        return rocketpy_flight
+
+    def get_flight_summary(self) -> FlightSummary:
+        """
+        Get the summary of the flight.
+
+        Returns:
+            FlightSummary
+        """
+        flight = self
+
+        _initial_conditions = InitialConditions(
+            initial_altitude="Attitude - e0: {:.3f} | e1: {:.3f} | e2: {:.3f} | e3: {:.3f}".format(
+                flight.e0(0), flight.e1(0), flight.e2(0), flight.e3(0)
+            ),
+            initial_velocity="Velocity - Vx: {:.2f} m/s | Vy: {:.2f} m/s | Vz: {:.2f} m/s".format(
+                flight.vx(0), flight.vy(0), flight.vz(0)
+            ),
+            initial_position="Position - x: {:.2f} m | y: {:.2f} m | z: {:.2f} m".format(
+                flight.x(0), flight.y(0), flight.z(0)
+            ),
+            initial_angular_position="Euler Angles - Spin φ : {:.2f}° | Nutation θ: {:.2f}° | Precession ψ: {:.2f}°".format(
+                flight.phi(0), flight.theta(0), flight.psi(0)
+            ),
+            initial_angular_velocity="Angular Velocity - ω1: {:.2f} rad/s | ω2: {:.2f} rad/s| ω3: {:.2f} rad/s".format(
+                flight.w1(0), flight.w2(0), flight.w3(0)
+            ),
+        )
+
+        _numerical_integration_settings = NumericalIntegrationSettings(
+            max_time="Maximum Allowed Flight Time: {:f} s".format(
+                flight.max_time
+            ),
+            max_time_step="Maximum Allowed Time Step: {:f} s".format(
+                flight.max_time_step
+            ),
+            min_time_step="Minimum Allowed Time Step: {:e} s".format(
+                flight.min_time_step
+            ),
+            relative_error_tolerance=f"Relative Error Tolerance: {flight.rtol}",
+            absolute_error_tolerance=f"Absolute Error Tolerance: {flight.atol}",
+            time_overshoot=f"Allow Event Overshoot: {flight.time_overshoot}",
+            terminate_on_apogee=f"Terminate Simulation on Apogee: {flight.terminate_on_apogee}",
+            number_of_time_steps=f"Number of Time Steps Used: {len(flight.time_steps)}",
+            function_evaluations_per_time_step=f"Number of Derivative Functions Evaluation: {sum(flight.function_evaluations_per_time_step)}",
+            avg_function_evaluations_per_time_step="Average Function Evaluations per Time Step: {:3f}".format(
+                sum(flight.function_evaluations_per_time_step)
+                / len(flight.time_steps)
+            ),
+        )
+
+        _launch_rail_conditions = LaunchRailConditions(
+            rail_length="Launch Rail Length: {:.2f} m".format(
+                flight.rail_length
+            ),
+            flight_inclination="Launch Rail Inclination: {:.2f}°".format(
+                flight.inclination
+            ),
+            flight_heading="Launch Rail Heading: {:.2f}°".format(
+                flight.heading
+            ),
+        )
+
+        _surface_wind_conditions = SurfaceWindConditions(
+            frontal_surface_wind_speed="Frontal Surface Wind Speed: {:.2f} m/s".format(
+                flight.frontal_surface_wind
+            ),
+            lateral_surface_wind_speed="Lateral Surface Wind Speed: {:.2f} m/s".format(
+                flight.lateral_surface_wind
+            ),
+        )
+
+        _out_of_rail_conditions = OutOfRailConditions(
+            out_of_rail_time="Rail Departure Time: {:.3f} s".format(
+                flight.out_of_rail_time
+            ),
+            out_of_rail_velocity="Rail Departure Velocity: {:.3f} m/s".format(
+                flight.out_of_rail_velocity
+            ),
+            out_of_rail_static_margin="Rail Departure Static Margin: {:.3f} c".format(
+                flight.rocket.static_margin(flight.out_of_rail_time)
+            ),
+            out_of_rail_angle_of_attack="Rail Departure Angle of Attack: {:.3f}°".format(
+                flight.angle_of_attack(flight.out_of_rail_time)
+            ),
+            out_of_rail_thrust_weight_ratio="Rail Departure Thrust-Weight Ratio: {:.3f}".format(
+                flight.rocket.thrust_to_weight(flight.out_of_rail_time)
+            ),
+            out_of_rail_reynolds_number="Rail Departure Reynolds Number: {:.3e}".format(
+                flight.reynolds_number(flight.out_of_rail_time)
+            ),
+        )
+
+        _burnout_conditions = BurnoutConditions(
+            burnout_time="Burn out time: {:.3f} s".format(
+                flight.rocket.motor.burn_out_time
+            ),
+            burnout_altitude="Altitude at burn out: {:.3f} m (AGL)".format(
+                flight.z(flight.rocket.motor.burn_out_time)
+                - flight.env.elevation
+            ),
+            burnout_rocket_velocity="Rocket velocity at burn out: {:.3f} m/s".format(
+                flight.speed(flight.rocket.motor.burn_out_time)
+            ),
+            burnout_freestream_velocity="Freestream velocity at burn out: {:.3f} m/s".format(
+                (
+                    flight.stream_velocity_x(flight.rocket.motor.burn_out_time)
+                    ** 2
+                    + flight.stream_velocity_y(
+                        flight.rocket.motor.burn_out_time
+                    )
+                    ** 2
+                    + flight.stream_velocity_z(
+                        flight.rocket.motor.burn_out_time
+                    )
+                    ** 2
+                )
+                ** 0.5
+            ),
+            burnout_mach_number="Mach Number at burn out: {:.3f}".format(
+                flight.mach_number(flight.rocket.motor.burn_out_time)
+            ),
+            burnout_kinetic_energy="Kinetic energy at burn out: {:.3e}".format(
+                flight.kinetic_energy(flight.rocket.motor.burn_out_time)
+            ),
+        )
+
+        _apogee_conditions = ApogeeConditions(
+            apogee_altitude="Apogee Altitude: {:.3f} m (ASL) | {:.3f} m (AGL)".format(
+                flight.apogee, flight.apogee - flight.env.elevation
+            ),
+            apogee_time="Apogee Time: {:.3f} s".format(flight.apogee_time),
+            apogee_freestream_speed="Apogee Freestream Speed: {:.3f} m/s".format(
+                flight.apogee_freestream_speed
+            ),
+        )
+
+        _maximum_values = MaximumValues(
+            maximum_speed="Maximum Speed: {:.3f} m/s at {:.2f} s".format(
+                flight.max_speed, flight.max_speed_time
+            ),
+            maximum_mach_number="Maximum Mach Number: {:.3f} Mach at {:.2f} s".format(
+                flight.max_mach_number, flight.max_mach_number_time
+            ),
+            maximum_reynolds_number="Maximum Reynolds Number: {:.3e} at {:.2f} s".format(
+                flight.max_reynolds_number, flight.max_reynolds_number_time
+            ),
+            maximum_dynamic_pressure="Maximum Dynamic Pressure: {:.3e} Pa at {:.2f} s".format(
+                flight.max_dynamic_pressure,
+                flight.max_dynamic_pressure_time,
+            ),
+            maximum_acceleration_during_motor_burn="Maximum Acceleration During Motor Burn: {:.3f} m/s² at {:.2f} s".format(
+                flight.max_acceleration, flight.max_acceleration_time
+            ),
+            maximum_gs_during_motor_burn="Maximum Gs During Motor Burn: {:.3f} g at {:.2f} s".format(
+                flight.max_acceleration
+                / flight.env.gravity(flight.z(flight.max_acceleration_time)),
+                flight.max_acceleration_time,
+            ),
+            maximum_acceleration_after_motor_burn="Maximum Acceleration After Motor Burn: {:.3f} m/s² at {:.2f} s".format(
+                flight.max_acceleration_power_off,
+                flight.max_acceleration_power_off_time,
+            ),
+            maximum_gs_after_motor_burn="Maximum Gs After Motor Burn: {:.3f} g at {:.2f} s".format(
+                flight.max_acceleration_power_off / flight.env.standard_g,
+                flight.max_acceleration_power_off_time,
+            ),
+            maximum_upper_rail_button_normal_force="Maximum Upper Rail Button Normal Force: {:.3f} N".format(
+                flight.max_rail_button1_normal_force
+            ),
+            maximum_upper_rail_button_shear_force="Maximum Upper Rail Button Shear Force: {:.3f} N".format(
+                flight.max_rail_button1_shear_force
+            ),
+            maximum_lower_rail_button_normal_force="Maximum Lower Rail Button Normal Force: {:.3f} N".format(
+                flight.max_rail_button2_normal_force
+            ),
+            maximum_lower_rail_button_shear_force="Maximum Lower Rail Button Shear Force: {:.3f} N".format(
+                flight.max_rail_button2_shear_force
+            ),
+        )
+
+        if len(flight.impact_state) != 0:
+            _impact_conditions = ImpactConditions(
+                x_impact_position="X Impact: {:.3f} m".format(flight.x_impact),
+                y_impact_position="Y Impact: {:.3f} m".format(flight.y_impact),
+                time_of_impact="Time of Impact: {:.3f} s".format(
+                    flight.t_final
+                ),
+                impact_velocity="Velocity at Impact: {:.3f} m/s".format(
+                    flight.impact_velocity
+                ),
+            )
+        elif flight.terminate_on_apogee is False:
+            _impact_conditions = ImpactConditions(
+                time="Time: {:.3f} s".format(flight.solution[-1][0]),
+                altitude="Altitude: {:.3f} m".format(flight.solution[-1][3]),
+            )
+
+        if len(flight.parachute_events) == 0:
+            _events_registered = EventsRegistered(
+                events_trace="No parachute event registered"
+            )
+        else:
+            events = {}
+            for event in flight.parachute_events:
+                trigger_time = event[0]
+                parachute = event[1]
+                open_time = trigger_time + parachute.lag
+                velocity = flight.free_stream_speed(open_time)
+                altitude = flight.z(open_time)
+                name = parachute.name.title()
+                events[name] = []
+                events[name].append(
+                    name
+                    + " Ejection Triggered at: {:.3f} s".format(trigger_time)
+                )
+                events[name].append(
+                    name + " Parachute Inflated at: {:.3f} s".format(open_time)
+                )
+                events[name].append(
+                    name
+                    + " Parachute Inflated with Freestream Speed of: {:.3f} m/s".format(
+                        velocity
+                    )
+                )
+                events[name].append(
+                    name
+                    + " Parachute Inflated at Height of: {:.3f} m (AGL)".format(
+                        altitude - flight.env.elevation
+                    )
+                )
+            _events_registered = EventsRegistered(events_trace=events)
+
+        _flight_data = FlightData(
+            initial_conditions=_initial_conditions,
+            numerical_integration_settings=_numerical_integration_settings,
+            surface_wind_conditions=_surface_wind_conditions,
+            launch_rail_conditions=_launch_rail_conditions,
+            out_of_rail_conditions=_out_of_rail_conditions,
+            burnout_conditions=_burnout_conditions,
+            apogee_conditions=_apogee_conditions,
+            maximum_values=_maximum_values,
+            impact_conditions=_impact_conditions,
+            events_registered=_events_registered,
+        )
+
+        flight_summary = FlightSummary(flight_data=_flight_data)
+        return flight_summary
diff --git a/lib/services/motor.py b/lib/services/motor.py
new file mode 100644
index 0000000..2b56e9f
--- /dev/null
+++ b/lib/services/motor.py
@@ -0,0 +1,103 @@
+from typing import Self
+from rocketpy.motors.motor import Motor as RocketPyMotor
+from rocketpy.motors.solid_motor import SolidMotor
+from rocketpy.motors.liquid_motor import LiquidMotor
+from rocketpy.motors.hybrid_motor import HybridMotor
+from rocketpy.utilities import get_instance_attributes
+from lib.models.motor import Motor, MotorKinds
+from lib.views.motor import MotorSummary, MotorData, MotorPlots
+
+
+class MotorService(RocketPyMotor):
+
+    @classmethod
+    def from_motor_model(cls, motor: Motor) -> Self:
+        """
+        Get the rocketpy motor object.
+
+        Returns:
+            RocketPyMotor
+        """
+
+        motor_core = {
+            "thrust_source": f"lib/data/engines/{motor.thrust_source.value}.eng",
+            "burn_time": motor.burn_time,
+            "nozzle_radius": motor.nozzle_radius,
+            "dry_mass": motor.dry_mass,
+            "dry_inertia": motor.dry_inertia,
+            "center_of_dry_mass_position": motor.center_of_dry_mass_position,
+        }
+
+        match motor.motor_kind:
+            case MotorKinds.LIQUID:
+                rocketpy_motor = LiquidMotor(**motor_core)
+            case MotorKinds.HYBRID:
+                rocketpy_motor = HybridMotor(
+                    **motor_core,
+                    throat_radius=motor.throat_radius,
+                    grain_number=motor.grain_number,
+                    grain_density=motor.grain_density,
+                    grain_outer_radius=motor.grain_outer_radius,
+                    grain_initial_inner_radius=motor.grain_initial_inner_radius,
+                    grain_initial_height=motor.grain_initial_height,
+                    grain_separation=motor.grain_separation,
+                    grains_center_of_mass_position=motor.grains_center_of_mass_position,
+                )
+            case _:
+                rocketpy_motor = SolidMotor(
+                    **motor_core,
+                    grain_number=motor.grain_number,
+                    grain_density=motor.grain_density,
+                    grain_outer_radius=motor.grain_outer_radius,
+                    grain_initial_inner_radius=motor.grain_initial_inner_radius,
+                    grain_initial_height=motor.grain_initial_height,
+                    grains_center_of_mass_position=motor.grains_center_of_mass_position,
+                    grain_separation=motor.grain_separation,
+                    throat_radius=motor.throat_radius,
+                    interpolation_method=motor.interpolation_method,
+                )
+
+        if motor.motor_kind != MotorKinds.SOLID:
+            for tank in motor.tanks:
+                rocketpy_motor.add_tank(tank.tank, tank.position)
+
+        return rocketpy_motor
+
+    def get_motor_summary(self) -> MotorSummary:
+        """
+        Get the summary of the motor.
+
+        Returns:
+            MotorSummary
+        """
+
+        motor_simulation_numbers = MotorData(
+            total_burning_time="Total Burning Time: "
+            + str(self.burn_out_time)
+            + " s",
+            total_propellant_mass="Total Propellant Mass: "
+            + "{:.3f}".format(self.propellant_initial_mass)
+            + " kg",
+            average_propellant_exhaust_velocity="Average Propellant Exhaust Velocity: "
+            + "{:.3f}".format(self.exhaust_velocity.average(*self.burn_time))
+            + " m/s",
+            average_thrust="Average Thrust: "
+            + "{:.3f}".format(self.average_thrust)
+            + " N",
+            maximum_thrust="Maximum Thrust: "
+            + str(self.max_thrust)
+            + " N at "
+            + str(self.max_thrust_time)
+            + " s after ignition.",
+            total_impulse="Total Impulse: "
+            + "{:.3f}".format(self.total_impulse)
+            + " Ns\n",
+        )
+        # motor_simulation_plots = MotorPlots(
+        #    self.thrust.plot(lower=lower_limit, upper=upper_limit)
+        # )
+        motor_summary = MotorSummary(
+            motor_data=motor_simulation_numbers
+        )  # , plots=motor_simulation_plots )
+
+        return motor_summary
diff --git a/lib/services/rocket.py b/lib/services/rocket.py
new file mode 100644
index 0000000..4bc604c
--- /dev/null
+++ b/lib/services/rocket.py
@@ -0,0 +1,371 @@
+import os
+import ast
+from typing import Self
+from rocketpy.rocket.rocket import Rocket as RocketPyRocket
+from rocketpy.rocket.parachute import Parachute as RocketPyParachute
+from rocketpy.rocket.aero_surface import NoseCone as RocketPyNoseCone
+from rocketpy.rocket.aero_surface import (
+    TrapezoidalFins as RocketPyTrapezoidalFins,
+)
+from rocketpy.rocket.aero_surface import Tail as RocketPyTail
+from rocketpy.utilities import get_instance_attributes
+
+from lib.models.rocket import Rocket
+from lib.models.aerosurfaces import NoseCone, TrapezoidalFins, Tail
+from lib.models.parachute import Parachute
+from lib.services.motor import MotorService
+from lib.views.rocket import (
+    InertiaDetails,
+    RocketGeometricalParameters,
+    RocketAerodynamicsQuantities,
+    ParachuteData,
+    RocketData,
+    RocketSummary,
+)
+
+
+class RocketService(RocketPyRocket):
+
+    @classmethod
+    def from_rocket_model(cls, rocket: Rocket) -> Self:
+        """
+        Get the rocketpy rocket object.
+
+        Returns:
+            RocketPyRocket
+        """
+
+        rocketpy_rocket = RocketPyRocket(
+            radius=rocket.radius,
+            mass=rocket.mass,
+            inertia=rocket.inertia,
+            power_off_drag=os.path.join(
+                "lib/data",
+                f"{rocket.rocket_option.lower()}",
+                "powerOffDragCurve.csv",
+            ),
+            power_on_drag=os.path.join(
+                "lib/data",
+                f"{rocket.rocket_option.lower()}",
+                "powerOnDragCurve.csv",
+            ),
+            center_of_mass_without_motor=rocket.center_of_mass_without_motor,
+            coordinate_system_orientation=rocket.coordinate_system_orientation,
+        )
+
+        # RailButtons
+        rocketpy_rocket.set_rail_buttons(
+            upper_button_position=rocket.rail_buttons.upper_button_position,
+            lower_button_position=rocket.rail_buttons.lower_button_position,
+            angular_position=rocket.rail_buttons.angular_position,
+        )
+        rocketpy_rocket.add_motor(
+            MotorService.from_motor_model(rocket.motor),
+            rocket.motor_position,
+        )
+
+        # NoseCone
+        nose = cls.get_rocketpy_nose(rocket.nose)
+        rocketpy_rocket.aerodynamic_surfaces.add(nose, nose.position)
+        rocketpy_rocket.evaluate_static_margin()
+
+        # FinSet
+        # TODO: re-write this to match overall fins not only TrapezoidalFins
+        # Maybe a strategy with different factory methods?
+        finset = cls.get_rocketpy_finset(rocket.fins)
+        rocketpy_rocket.aerodynamic_surfaces.add(finset, finset.position)
+        rocketpy_rocket.evaluate_static_margin()
+
+        # Tail
+        tail = cls.get_rocketpy_tail(rocket.tail)
+        rocketpy_rocket.aerodynamic_surfaces.add(tail, tail.position)
+        rocketpy_rocket.evaluate_static_margin()
+
+        # Parachutes
+        for p, _ in enumerate(rocket.parachutes):
+            parachute_trigger = rocket.parachutes[p].triggers[0]
+            if cls.check_parachute_trigger(parachute_trigger):
+                rocket.parachutes[p].triggers[0] = compile(
+                    parachute_trigger, "<string>", "eval"
+                )
+                parachute = cls.get_rocketpy_parachute(rocket.parachutes, p)
+                rocketpy_rocket.parachutes.append(parachute)
+            else:
+                print("Parachute trigger not valid. Skipping parachute.")
+                continue
+
+        return rocketpy_rocket
+
+    def get_rocket_summary(self) -> RocketSummary:
+        """
+        Get the summary of the rocket.
+
+        Returns:
+            RocketSummary
+        """
+
+        _inertia_details = InertiaDetails(
+            rocket_mass_without_propellant="Rocket Mass: {:.3f} kg (No Propellant)".format(
+                self.mass
+            ),
+            rocket_mass_with_propellant="Rocket Mass: {:.3f} kg (With Propellant)".format(
+                self.total_mass(0)
+            ),
+            rocket_inertia_with_motor_without_propellant=[
+                "Rocket Inertia (with motor, but without propellant) 11: {:.3f} kg*m2".format(
+                    self.dry_I_11
+                ),
+                "Rocket Inertia (with motor, but without propellant) 22: {:.3f} kg*m2".format(
+                    self.dry_I_22
+                ),
+                "Rocket Inertia (with motor, but without propellant) 33: {:.3f} kg*m2".format(
+                    self.dry_I_33
+                ),
+                "Rocket Inertia (with motor, but without propellant) 12: {:.3f} kg*m2".format(
+                    self.dry_I_12
+                ),
+                "Rocket Inertia (with motor, but without propellant) 13: {:.3f} kg*m2".format(
+                    self.dry_I_13
+                ),
+                "Rocket Inertia (with motor, but without propellant) 23: {:.3f} kg*m2".format(
+                    self.dry_I_23
+                ),
+            ],
+        )
+
+        _rocket_geometrical_parameters = RocketGeometricalParameters(
+            rocket_maximum_radius="Rocket Maximum Radius: "
+            + str(self.radius)
+            + " m",
+            rocket_frontal_area="Rocket Frontal Area: "
+            + "{:.6f}".format(self.area)
+            + " m2",
+            rocket_codm_nozzle_exit_distance="Rocket Center of Dry Mass - Nozzle Exit Distance: "
+            + "{:.3f} m".format(
+                abs(self.center_of_dry_mass_position - self.motor_position)
+            ),
+            rocket_codm_center_of_propellant_mass="Rocket Center of Dry Mass - Center of Propellant Mass: "
+            + "{:.3f} m".format(
+                abs(
+                    self.center_of_propellant_position(0)
+                    - self.center_of_dry_mass_position
+                )
+            ),
+            rocket_codm_loaded_center_of_mass="Rocket Center of Mass - Rocket Loaded Center of Mass: "
+            + "{:.3f} m".format(
+                abs(self.center_of_mass(0) - self.center_of_dry_mass_position)
+            ),
+        )
+
+        _aerodynamics_lift_coefficient_derivatives = {}
+        for surface, _position in self.aerodynamic_surfaces:
+            name = surface.name
+            _aerodynamics_lift_coefficient_derivatives[name] = []
+            _aerodynamics_lift_coefficient_derivatives[name].append(
+                name
+                + " Lift Coefficient Derivative: {:.3f}".format(
+                    surface.clalpha(0)
+                )
+                + "/rad"
+            )
+
+        _aerodynamics_center_of_pressure = {}
+        for surface, _position in self.aerodynamic_surfaces:
+            name = surface.name
+            cpz = surface.cp[2]
+            _aerodynamics_center_of_pressure[name] = []
+            _aerodynamics_center_of_pressure[name].append(
+                name + " Center of Pressure to CM: {:.3f}".format(cpz) + " m"
+            )
+
+        _rocket_aerodynamics_quantities = RocketAerodynamicsQuantities(
+            aerodynamics_lift_coefficient_derivatives=_aerodynamics_lift_coefficient_derivatives,
+            aerodynamics_center_of_pressure=_aerodynamics_center_of_pressure,
+            distance_cop_to_codm="Distance from Center of Pressure to Center of Dry Mass: "
+            + "{:.3f}".format(self.center_of_mass(0) - self.cp_position(0))
+            + " m",
+            initial_static_margin="Initial Static Margin: "
+            + "{:.3f}".format(self.static_margin(0))
+            + " c",
+            final_static_margin="Final Static Margin: "
+            + "{:.3f}".format(self.static_margin(self.motor.burn_out_time))
+            + " c",
+        )
+
+        _parachute_details = {}
+        _parachute_ejection_signal_trigger = {}
+        _parachute_ejection_system_refresh_rate = {}
+        _parachute_lag = {}
+        for chute in self.parachutes:
+            _parachute_details[chute.name] = chute.__str__()
+
+            if chute.trigger.__name__ == "<lambda>":
+                # line = getsourcelines(chute.trigger)[0][0]
+                # _parachute_ejection_signal_trigger[chute.name] = "Ejection signal trigger: " + line.split("lambda ")[1].split(",")[0].split("\n")[0]
+                pass
+
+            else:
+                _parachute_ejection_signal_trigger[chute.name] = (
+                    "Ejection signal trigger: " + chute.trigger.__name__
+                )
+                _parachute_ejection_system_refresh_rate[chute.name] = (
+                    "Ejection system refresh rate: {chute.sampling_rate:.3f} Hz"
+                )
+                _parachute_lag[chute.name] = (
+                    "Time between ejection signal is triggered and the parachute is fully opened: {chute.lag:.1f} s\n"
+                )
+
+        _parachute_data = ParachuteData(
+            parachute_details=_parachute_details,
+            # parachute_ejection_signal_trigger = _parachute_ejection_signal_trigger,
+            parachute_ejection_system_refresh_rate=_parachute_ejection_system_refresh_rate,
+            parachute_lag=_parachute_lag,
+        )
+
+        _rocket_data = RocketData(
+            inertia_details=_inertia_details,
+            rocket_geometrical_parameters=_rocket_geometrical_parameters,
+            rocket_aerodynamics_quantities=_rocket_aerodynamics_quantities,
+            parachute_data=_parachute_data,
+        )
+
+        rocket_summary = RocketSummary(rocket_data=_rocket_data)
+        return rocket_summary
+
+    @staticmethod
+    def get_rocketpy_nose(nose: NoseCone) -> RocketPyNoseCone:
+        """
+        Get a rocketpy nose cone object.
+
+        Returns:
+            RocketPyNoseCone
+        """
+
+        rocketpy_nose = RocketPyNoseCone(
+            length=nose.length,
+            kind=nose.kind,
+            base_radius=nose.base_radius,
+            rocket_radius=nose.rocket_radius,
+        )
+        rocketpy_nose.position = nose.position
+        return rocketpy_nose
+
+    @staticmethod
+    def get_rocketpy_finset(
+        trapezoidal_fins: TrapezoidalFins,
+    ) -> RocketPyTrapezoidalFins:
+        """
+        Get a rocketpy finset object.
+
+        Returns:
+            RocketPyTrapezoidalFins
+        """
+        rocketpy_finset = RocketPyTrapezoidalFins(
+            n=trapezoidal_fins.n,
+            root_chord=trapezoidal_fins.root_chord,
+            tip_chord=trapezoidal_fins.tip_chord,
+            span=trapezoidal_fins.span,
+            cant_angle=trapezoidal_fins.cant_angle,
+            rocket_radius=trapezoidal_fins.radius,
+            airfoil=trapezoidal_fins.airfoil,
+        )
+        rocketpy_finset.position = trapezoidal_fins.position
+        return rocketpy_finset
+
+    @staticmethod
+    def get_rocketpy_tail(tail: Tail) -> RocketPyTail:
+        """
+        Get a rocketpy tail object.
+
+        Returns:
+            RocketPyTail
+        """
+        rocketpy_tail = RocketPyTail(
+            top_radius=tail.top_radius,
+            bottom_radius=tail.bottom_radius,
+            length=tail.length,
+            rocket_radius=tail.radius,
+        )
+        rocketpy_tail.position = tail.position
+        return rocketpy_tail
+
+    @staticmethod
+    def get_rocketpy_parachute(
+        parachute: Parachute, p: int
+    ) -> RocketPyParachute:
+        """
+        Get a rocketpy parachute object.
+
+        Returns:
+            RocketPyParachute
+        """
+        rocketpy_parachute = RocketPyParachute(
+            name=parachute[p].name[0],
+            cd_s=parachute[p].cd_s[0],
+            trigger=eval(parachute[p].triggers[0]),
+            sampling_rate=parachute[p].sampling_rate[0],
+            lag=parachute[p].lag[0],
+            noise=parachute[p].noise[0],
+        )
+        return rocketpy_parachute
+
+    @staticmethod
+    def check_parachute_trigger(expression: str) -> bool:
+        """
+        Check if the trigger expression is valid.
+
+        Args:
+            expression: str
+
+        Returns:
+            bool: True if the expression is valid, False otherwise.
+        """
+
+        # Parsing the expression into an AST
+        try:
+            parsed_expression = ast.parse(expression, mode="eval")
+        except SyntaxError:
+            print("Invalid syntax.")
+            return False
+
+        # Constant case (supported after beta v1)
+        if isinstance(parsed_expression.body, ast.Constant):
+            return True
+        # Name case (supported after beta v1)
+        if (
+            isinstance(parsed_expression.body, ast.Name)
+            and parsed_expression.body.id == "apogee"
+        ):
+            global apogee
+            apogee = "apogee"
+            return True
+
+        # Validating the expression structure
+        if not isinstance(parsed_expression.body, ast.Lambda):
+            print("Invalid expression structure (not a Lambda).")
+            return False
+
+        lambda_node = parsed_expression.body
+        if len(lambda_node.args.args) != 3:
+            print("Invalid expression structure (invalid arity).")
+            return False
+
+        if not isinstance(lambda_node.body, ast.Compare):
+            try:
+                for operand in lambda_node.body.values:
+                    if not isinstance(operand, ast.Compare):
+                        print("Invalid expression structure (not a Compare).")
+                        return False
+            except AttributeError:
+                print("Invalid expression structure (not a Compare).")
+                return False
+
+        # Restricting access to functions or attributes
+        for node in ast.walk(lambda_node):
+            if isinstance(node, ast.Call):
+                print("Calling functions is not allowed in the expression.")
+                return False
+            if isinstance(node, ast.Attribute):
+                print("Accessing attributes is not allowed in the expression.")
+                return False
+        return True
diff --git a/lib/views/environment.py b/lib/views/environment.py
index 15157db..e865e43 100644
--- a/lib/views/environment.py
+++ b/lib/views/environment.py
@@ -1,4 +1,3 @@
-from typing import List
 from pydantic import BaseModel
 
 
diff --git a/pyproject.toml b/pyproject.toml
index 190673c..3737d6e 100644
--- a/pyproject.toml
+++ b/pyproject.toml
@@ -7,7 +7,7 @@ dependencies = {file = ["requirements.txt"]}
 
 [project]
 name = "Infinity-API"
-version = "1.2.2"
+version = "2.0.0"
 description = "RESTFULL open API for rocketpy"
 dynamic = ["dependencies"]
 requires-python = ">=3.12"
@@ -55,5 +55,6 @@ disable = """
     wrong-import-position,
     consider-using-f-string,
     too-many-function-args,
-    no-member
+    no-member,
+    attribute-defined-outside-init
 """
diff --git a/tests/Infinity-API.postman_collection.json b/tests/Infinity-API.postman_collection.json
deleted file mode 100644
index 4ff23fc..0000000
--- a/tests/Infinity-API.postman_collection.json
+++ /dev/null
@@ -1,4304 +0,0 @@
-{
-	"info": {
-		"_postman_id": "00c970b2-c429-4ecd-a1f7-de23aa286d10",
-		"name": "Infinity-API",
-		"description": "# About this collection\n\nThe API under this collection includes four artifacts **{Environment, Flight, Motor and Rocket}** with 6 endpoints each covering artifact **creation, reading, editing, deleting, simulating and retrieving artifact as jsonpickle string.**\n\n- POST `api/artifact/{{artifact_id}}` { message, artifact_id }\n- GET `api/artifact/{{artifact_id}}` { Artifact }\n- GET `api/rocketpy/artifact/{{artifact_id}}` { json_pickle_string_artifact }\n- GET `api/simulate/artifact/{{artifact_id}}` { ArtifactSimulationSummary }\n- PUT `api/artifact/{{artifact_id}}` { message, new_artifact_id }\n- DELETE `api/artifact/{{artifact_id}}` { deleted_artifact_id, message }\n    \n\n**Flight artifact** have also additional routes that allows to update its own artifacts.\n\n- POST `api/flight/{{flight_id}}/artifact/` { message, flight_id }\n    \n\n## **Using this collection**\n\n- Run this collection by clicking on \"Run\".\n    \n\n<img src=\"https://content.pstmn.io/84019b0f-69c8-4c5f-98b9-2c90a6f9a0b1/Y29sbGVjdGlvbi1ydW5uZXItYnV0dG9uLmpwZWc=\" width=\"266\" height=\"103\">\n\n## Additional resources\n\n[Scripting in Postman](https://learning.postman.com/docs/writing-scripts/intro-to-scripts/)\n\n[Test script examples](https://learning.postman.com/docs/writing-scripts/script-references/test-examples/)\n\n[Postman Sandbox API reference](https://learning.postman.com/docs/sending-requests/grpc/postman-sandbox-api/#writing-assertions)\n\n[Using the Collection Runner](https://learning.postman.com/docs/collections/running-collections/intro-to-collection-runs/)",
-		"schema": "https://schema.getpostman.com/json/collection/v2.1.0/collection.json",
-		"_exporter_id": "29631298",
-		"_collection_link": "https://rocketpy-team.postman.co/workspace/Team-Workspace~d228e0d7-1148-4935-8e58-7db52744ee04/collection/29631298-00c970b2-c429-4ecd-a1f7-de23aa286d10?action=share&source=collection_link&creator=29631298"
-	},
-	"item": [
-		{
-			"name": "Environment",
-			"item": [
-				{
-					"name": "Create Environment",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"var envRequest = JSON.parse(pm.request.body.raw);",
-									"",
-									"// reduce date for future assert",
-									"envRequest.date = envRequest.date.substring(0, envRequest.date.length - 7);",
-									"",
-									"// save environment parameters",
-									"pm.environment.set('env_id', apiRspn.env_id)        ",
-									"pm.environment.set('latitude', envRequest.latitude)",
-									"pm.environment.set('longitude', envRequest.longitude)",
-									"pm.environment.set('elevation', envRequest.elevation)      ",
-									"pm.environment.set('atmospheric_model_type', envRequest.atmospheric_model_type)    ",
-									"pm.environment.set('atmospheric_model_file', envRequest.atmospheric_model_file)            ",
-									"pm.environment.set('date', envRequest.date)        ",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid environment POST request is made to the API\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Environment successfully created\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid env_id\", function () {",
-									"        pm.expect(apiRspn.env_id).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						},
-						{
-							"listen": "prerequest",
-							"script": {
-								"exec": [
-									""
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "POST",
-						"header": [],
-						"body": {
-							"mode": "raw",
-							"raw": "{\n    \"latitude\": 0,\n    \"longitude\": 0,\n    \"elevation\": 1400,\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"atmospheric_model_file\": \"GFS\",\n    \"date\": \"2023-05-09T16:30:50.065992\"\n}",
-							"options": {
-								"raw": {
-									"language": "json"
-								}
-							}
-						},
-						"url": {
-							"raw": "{{endpoint}}/environments/",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"environments",
-								""
-							]
-						},
-						"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-					},
-					"response": []
-				},
-				{
-					"name": "Read Environment",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"",
-									"var returned_date = apiRspn.date;",
-									"var reduced_returned_date = returned_date.substring(0, returned_date.length - 7);",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Environment GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid environment\", function () {",
-									"        pm.expect(apiRspn.latitude).to.eql(pm.environment.get('latitude'), \"latitude not matching\");",
-									"        pm.expect(apiRspn.longitude).to.eql(pm.environment.get('longitude'), \"longitude not matching\");        ",
-									"        pm.expect(apiRspn.elevation).to.eql(pm.environment.get('elevation'), \"elevation not matching\");",
-									"        pm.expect(apiRspn.atmospheric_model_type).to.eql(pm.environment.get('atmospheric_model_type'), \"atmospheric_model_type not matching\");",
-									"        pm.expect(apiRspn.atmospheric_model_file).to.eql(pm.environment.get('atmospheric_model_file'), \"atmospheric_model_file not matching\");",
-									"        pm.expect(reduced_returned_date).to.eql(pm.environment.get('date'), \"date not matching\");",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/environments/{{env_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"environments",
-								"{{env_id}}"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Read rocketpy Environment",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid rocketpy Environment GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.jsonpickle_rocketpy_env).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/environments/rocketpy/{{env_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"environments",
-								"rocketpy",
-								"{{env_id}}"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Simulate Environment",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"//TEST",
-									"bdd = \"Given a valid rocketpy Environment simulate GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.env_data).to.exist;        ",
-									"        //pm.expect(apiRspn.env_data.grav).to.exist;   ",
-									"        pm.expect(apiRspn.env_data.wind_speed).to.exist;",
-									"        pm.expect(apiRspn.env_data.model_type_max_expected_height).to.exist;",
-									"        pm.expect(apiRspn.env_data.wind_speed).to.exist;",
-									"        pm.expect(apiRspn.env_data.wind_direction).to.exist;",
-									"        pm.expect(apiRspn.env_data.wind_heading).to.exist;",
-									"        pm.expect(apiRspn.env_data.surface_pressure).to.exist;",
-									"        pm.expect(apiRspn.env_data.surface_temperature).to.exist;",
-									"        pm.expect(apiRspn.env_data.surface_air_density).to.exist;",
-									"        pm.expect(apiRspn.env_data.surface_speed_of_sound).to.exist;",
-									"        pm.expect(apiRspn.env_data.launch_date).to.exist;",
-									"        pm.expect(apiRspn.env_data.lat).to.eql(pm.environment.get('latitude'), \"latitude not matching\");",
-									"        pm.expect(apiRspn.env_data.lon).to.eql(pm.environment.get('longitude'), \"longitude not matching\");        ",
-									"        pm.expect(apiRspn.env_data.elevation).to.eql(pm.environment.get('elevation'), \"elevation not matching\");",
-									"        pm.expect(apiRspn.env_data.model_type).to.eql(pm.environment.get('atmospheric_model_type'), \"atmospheric_model_type not matching\");      ",
-									"",
-									"        pm.expect(apiRspn.env_plots).to.exist;     ",
-									"        pm.expect(apiRspn.env_plots.grid).to.exist;",
-									"        pm.expect(apiRspn.env_plots.wind_speed).to.exist;",
-									"        pm.expect(apiRspn.env_plots.wind_direction).to.exist;",
-									"        pm.expect(apiRspn.env_plots.speed_of_sound).to.exist;",
-									"        pm.expect(apiRspn.env_plots.density).to.exist;",
-									"        pm.expect(apiRspn.env_plots.wind_vel_x).to.exist;",
-									"        pm.expect(apiRspn.env_plots.wind_vel_y).to.exist;",
-									"        pm.expect(apiRspn.env_plots.pressure).to.exist;",
-									"        pm.expect(apiRspn.env_plots.temperature).to.exist;",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/environments/{{env_id}}/simulate",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"environments",
-								"{{env_id}}",
-								"simulate"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Update Environment",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"var envRequest = JSON.parse(pm.request.body.raw);",
-									"",
-									"// reduce date for future assert",
-									"envRequest.date = envRequest.date.substring(0, envRequest.date.length - 7);",
-									"",
-									"// save environment parameters",
-									"pm.environment.set('env_id', apiRspn.new_env_id)        ",
-									"pm.environment.set('latitude', envRequest.latitude)",
-									"pm.environment.set('longitude', envRequest.longitude)",
-									"pm.environment.set('elevation', envRequest.elevation)      ",
-									"pm.environment.set('atmospheric_model_type', envRequest.atmospheric_model_type)    ",
-									"pm.environment.set('atmospheric_model_file', envRequest.atmospheric_model_file)            ",
-									"pm.environment.set('date', envRequest.date)        ",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Environment PUT request is made to the API\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Environment successfully updated\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid new_env_id\", function () {",
-									"        pm.expect(apiRspn.new_env_id).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						},
-						{
-							"listen": "prerequest",
-							"script": {
-								"exec": [
-									""
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "PUT",
-						"header": [],
-						"body": {
-							"mode": "raw",
-							"raw": "{\n    \"latitude\": 0,\n    \"longitude\": 0,\n    \"elevation\": 1400,\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"atmospheric_model_file\": \"GFS\",\n    \"date\": \"2023-05-09T16:30:50.065992\"\n}",
-							"options": {
-								"raw": {
-									"language": "json"
-								}
-							}
-						},
-						"url": {
-							"raw": "{{endpoint}}/environments/{{env_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"environments",
-								"{{env_id}}"
-							]
-						},
-						"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-					},
-					"response": []
-				},
-				{
-					"name": "Delete Environment",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"//TEST",
-									"bdd = \"Given a valid Environment DELETE request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Environment successfully deleted\", \"message not matching\");",
-									"        pm.expect(apiRspn.deleted_env_id).to.eql(pm.environment.get('env_id'), \"env_id not matching\");                ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "DELETE",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/environments/{{env_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"environments",
-								"{{env_id}}"
-							]
-						}
-					},
-					"response": []
-				}
-			]
-		},
-		{
-			"name": "Flight",
-			"item": [
-				{
-					"name": "Hybrid",
-					"item": [
-						{
-							"name": "Create Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// reduce environment date for future assertion",
-											"flightRequest.environment.date = flightRequest.environment.date.substring(0, flightRequest.environment.date.length - 7);",
-											"",
-											"// save flight parameters",
-											"pm.environment.set('rail_length', flightRequest.rail_length)        ",
-											"pm.environment.set('inclination', flightRequest.inclination)",
-											"pm.environment.set('heading', flightRequest.heading)",
-											"",
-											"// flight environment",
-											"pm.environment.set('flight_id', apiRspn.flight_id)        ",
-											"pm.environment.set('latitude', flightRequest.environment.latitude)",
-											"pm.environment.set('longitude', flightRequest.environment.longitude)",
-											"pm.environment.set('elevation', flightRequest.environment.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.environment.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.environment.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.environment.date)        ",
-											"",
-											"// flight rocket",
-											"pm.environment.set('radius', flightRequest.rocket.radius)",
-											"pm.environment.set('mass', flightRequest.rocket.mass)",
-											"pm.environment.set('inertia', flightRequest.rocket.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.rocket.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.rocket.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.rocket.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.rocket.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rocket.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rocket.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rocket.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rocket.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.rocket.coordinate_system_orientation)",
-											"",
-											"// flight rocket motor",
-											"pm.environment.set('burn_time', flightRequest.rocket.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.rocket.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.rocket.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.rocket.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.rocket.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.rocket.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.rocket.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.rocket.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.rocket.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.rocket.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.rocket.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.rocket.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.rocket.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.rocket.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.rocket.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.rocket.motor.coordinate_system_orientation)",
-											"",
-											"// flight rocket nose",
-											"pm.environment.set('nose_length', flightRequest.rocket.nose.length)",
-											"pm.environment.set('kind', flightRequest.rocket.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.rocket.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.rocket.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.rocket.nose.rocket_radius)",
-											"",
-											"// flight rocket fins",
-											"pm.environment.set('n', flightRequest.rocket.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.rocket.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.rocket.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.rocket.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.rocket.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.rocket.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.rocket.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.rocket.fins.airfoil)",
-											"",
-											"// flight rocket tail",
-											"pm.environment.set('top_radius', flightRequest.rocket.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.rocket.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.rocket.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.rocket.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.rocket.tail.radius)",
-											"",
-											"// flight rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.rocket.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.rocket.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.rocket.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.rocket.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.rocket.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.rocket.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight POST request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully created\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight_id\", function () {",
-											"        pm.expect(apiRspn.flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "POST",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"environment\": {\n    \"atmospheric_model_file\": \"GFS\",\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"date\": \"2023-12-29T10:22:00.921396\",\n    \"elevation\": 1400,\n    \"latitude\": 0,\n    \"longitude\": 0\n  },\n  \"rocket\": {\n    \"center_of_mass_without_motor\": 0,\n    \"coordinate_system_orientation\": \"tail_to_nose\",\n    \"fins\": {\n      \"airfoil\": \"\",\n      \"cant_angle\": 0,\n      \"n\": 4,\n      \"position\": -1.04956,\n      \"radius\": 0.0635,\n      \"root_chord\": 0.12,\n      \"span\": 0.1,\n      \"tip_chord\": 0.04\n    },\n    \"inertia\": [\n      6.321,\n      6.321,\n      0.0346\n    ],\n    \"mass\": 16.235,\n    \"motor\": {\n      \"burn_time\": 3.9,\n      \"center_of_dry_mass_position\": 0.317,\n      \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n      \"dry_inertia\": [\n        0.125,\n        0.125,\n        0.002\n      ],\n      \"dry_mass\": 1.815,\n      \"grain_density\": 1815,\n      \"grain_initial_height\": 0.12,\n      \"grain_initial_inner_radius\": 0.015,\n      \"grain_number\": 5,\n      \"grain_outer_radius\": 0.033,\n      \"grain_separation\": 0.005,\n      \"grains_center_of_mass_position\": -0.85704,\n      \"interpolation_method\": \"linear\",\n      \"nozzle_radius\": 0.033,\n      \"tanks\": [\n        {\n          \"discretize\": 100,\n          \"flux_time\": [\n            0,\n            8\n          ],\n          \"gas\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"gas_mass\": 0.1,\n          \"gas_mass_flow_rate_in\": 0.1,\n          \"gas_mass_flow_rate_out\": 0.1,\n          \"geometry\": [\n            [\n              [\n                0,\n                5\n              ],\n              1\n            ],\n            [\n              [\n                5,\n                10\n              ],\n              2\n            ]\n          ],\n          \"initial_gas_mass\": 0.1,\n          \"initial_liquid_mass\": 5,\n          \"liquid\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"liquid_height\": 0.5,\n          \"liquid_mass\": 5,\n          \"liquid_mass_flow_rate_in\": 0.1,\n          \"liquid_mass_flow_rate_out\": 0.1,\n          \"name\": \"Tank\",\n          \"position\": 1,\n          \"tank_kind\": \"MassFlow\",\n          \"ullage\": 0.1\n        }\n      ],\n      \"throat_radius\": 0.011,\n      \"thrust_source\": \"Cesaroni_M1670\"\n    },\n    \"motor_position\": -1.255,\n    \"nose\": {\n      \"base_radius\": 0.0635,\n      \"kind\": \"vonKarman\",\n      \"length\": 0.55829,\n      \"position\": 1.278,\n      \"rocket_radius\": 0.0635\n    },\n    \"parachutes\": {\n      \"cd_s\": [\n        10,\n        1\n      ],\n      \"lag\": [\n        1.5,\n        1.5\n      ],\n      \"name\": [\n        \"Main\",\n        \"Drogue\"\n      ],\n      \"noise\": [\n        [\n          0,\n          8.3,\n          0.5\n        ],\n        [\n          0,\n          8.3,\n          0.5\n        ]\n      ],\n      \"sampling_rate\": [\n        105,\n        105\n      ],\n      \"triggers\": [\n        \"lambda p, h, y: y[5] < 0 and h < 800\",\n        \"lambda p, h, y: y[5] < 0\"\n      ]\n    },\n    \"power_off_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"power_on_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"radius\": 0.0632,\n    \"rail_buttons\": {\n      \"angular_position\": 45,\n      \"lower_button_position\": 0.2,\n      \"upper_button_position\": -0.5\n    },\n    \"tail\": {\n      \"bottom_radius\": 0.0435,\n      \"length\": 0.06,\n      \"position\": -1.194656,\n      \"radius\": 0.0635,\n      \"top_radius\": 0.0635\n    }\n  },\n  \"inclination\": 85,\n  \"heading\": 0,\n  \"rail_length\": 5.2\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/?rocket_option=Calisto&motor_kind=Hybrid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										""
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Hybrid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Read Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"",
-											"var returned_date = apiRspn.environment.date;",
-											"var reduced_returned_date = returned_date.substring(0, returned_date.length - 7);",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight \", function () {",
-											"        pm.expect(apiRspn.inclination).to.eql(pm.environment.get('inclination'), \"flight inclination not matching\");",
-											"        pm.expect(apiRspn.heading).to.eql(pm.environment.get('heading'), \"flight heading not matching\");",
-											"        pm.expect(apiRspn.rail_length).to.eql(pm.environment.get('rail_length'), \"flight rail_length not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight environment\", function () {",
-											"        pm.expect(apiRspn.environment.longitude).to.eql(pm.environment.get('longitude'), \"environment longitude not matching\");        ",
-											"        pm.expect(apiRspn.environment.elevation).to.eql(pm.environment.get('elevation'), \"environment elevation not matching\");",
-											"        pm.expect(apiRspn.environment.atmospheric_model_type).to.eql(pm.environment.get('atmospheric_model_type'), \"environment atmospheric_model_type not matching\");",
-											"        pm.expect(apiRspn.environment.atmospheric_model_file).to.eql(pm.environment.get('atmospheric_model_file'), \"environment atmospheric_model_file not matching\");",
-											"        pm.expect(reduced_returned_date).to.eql(pm.environment.get('date'), \"date not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket\", function () {        ",
-											"        pm.expect(apiRspn.rocket.radius).to.eql(pm.environment.get('radius'), \"rocket radius not matching\");",
-											"        pm.expect(apiRspn.rocket.mass).to.eql(pm.environment.get('mass'), \"rocket mass not matching\");",
-											"        pm.expect(apiRspn.rocket.inertia).to.eql(pm.environment.get('inertia'), \"rocket inertia not matching\");",
-											"        pm.expect(apiRspn.rocket.power_off_drag).to.eql(pm.environment.get('power_off_drag'), \"rocket power_off_drag not matching\");",
-											"        pm.expect(apiRspn.rocket.power_on_drag).to.eql(pm.environment.get('power_on_drag'), \"rocket power_on_drag not matching\");",
-											"        pm.expect(apiRspn.rocket.center_of_mass_without_motor).to.eql(pm.environment.get('center_of_mass_without_motor'), \"rocket center_of_mass_without_motor not matching\");",
-											"        pm.expect(apiRspn.rocket.coordinate_system_orientation).to.eql(pm.environment.get('rocket_coordinate_system_orientation'), \"rocket coordinate_system_orientation not matching\");",
-											"        pm.expect(apiRspn.rocket.motor_position).to.eql(pm.environment.get('motor_position'), \"rocket motor_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons).to.eql(pm.environment.get('rail_buttons'), \"rocket rail_buttons not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.upper_button_position).to.eql(pm.environment.get('upper_button_position'), \"rocket rail_buttons upper_button_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.lower_button_position).to.eql(pm.environment.get('lower_button_position'), \"rocket rail_buttons lower_button_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.angular_position).to.eql(pm.environment.get('angular_position'), \"rocket rail_buttons angular_position not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket motor\", function () {",
-											"        pm.expect(apiRspn.rocket.motor.burn_time).to.eql(pm.environment.get('burn_time'), \"rocket motor burn_time not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.dry_mass).to.eql(pm.environment.get('dry_mass'), \"rocket motor dry_mass not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.dry_inertia).to.eql(pm.environment.get('dry_inertia'), \"rocket motor dry_inertia not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.center_of_dry_mass_position).to.eql(pm.environment.get('center_of_dry_mass_position'), \"rocket motor center_of_dry_mass_position not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_number).to.eql(pm.environment.get('grain_number'), \"rocket motor grain_number not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_density).to.eql(pm.environment.get('grain_density'), \"rocket motor grain_density not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_outer_radius).to.eql(pm.environment.get('grain_outer_radius'), \"rocket motor grain_outer_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_initial_inner_radius).to.eql(pm.environment.get('grain_initial_inner_radius'), \"rocket motor grain_initial_inner_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_initial_height).to.eql(pm.environment.get('grain_initial_height'), \"rocket motor grain_initial_height not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grains_center_of_mass_position).to.eql(pm.environment.get('grains_center_of_mass_position'), \"rocket motor grains_center_of_mass_position not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.thrust_source).to.eql(pm.environment.get('thrust_source'), \"rocket motor thrust_source not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_separation).to.eql(pm.environment.get('grain_separation'), \"rocket motor grain_separation not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.nozzle_radius).to.eql(pm.environment.get('nozzle_radius'), \"rocket motor nozzle_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.throat_radius).to.eql(pm.environment.get('throat_radius'), \"rocket motor throat_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.interpolation_method).to.eql(pm.environment.get('interpolation_method'), \"rocket motor interpolation_method not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.coordinate_system_orientation).to.eql(pm.environment.get('motor_coordinate_system_orientation'), \"motor coordinate_system_orientation not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket nose\", function () {",
-											"        pm.expect(apiRspn.rocket.nose.length).to.eql(pm.environment.get('nose_length'), \"rocket nose length not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.kind).to.eql(pm.environment.get('kind'), \"rocket nose kind not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.position).to.eql(pm.environment.get('nose_position'), \"rocket nose position not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.base_radius).to.eql(pm.environment.get('base_radius'), \"rocket nose base_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.rocket_radius).to.eql(pm.environment.get('rocket_radius'), \"rocket nose rocket_radius not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket fins\", function () {",
-											"        pm.expect(apiRspn.rocket.fins.n).to.eql(pm.environment.get('n'), \"rocket fins 'n' not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.root_chord).to.eql(pm.environment.get('root_chord'), \"rocket fins root_chord not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.tip_chord).to.eql(pm.environment.get('tip_chord'), \"rocket fins tip_chord not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.span).to.eql(pm.environment.get('span'), \"rocket fins span not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.position).to.eql(pm.environment.get('fin_position'), \"rocket fins position not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.cant_angle).to.eql(pm.environment.get('cant_angle'), \"rocket fins cant_angle not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.radius).to.eql(pm.environment.get('fin_radius'), \"rocket fins radius not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.airfoil).to.eql(pm.environment.get('airfoil'), \"rocket fins airfoil not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket tail\", function () {",
-											"        pm.expect(apiRspn.rocket.tail.top_radius).to.eql(pm.environment.get('top_radius'), \"rocket tail top_radius not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.bottom_radius).to.eql(pm.environment.get('bottom_radius'), \"rocket tail bottom_radius not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.length).to.eql(pm.environment.get('tail_length'), \"rocket tail length not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.position).to.eql(pm.environment.get('tail_position'), \"rocket tail position not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.radius).to.eql(pm.environment.get('tail_radius'), \"rocket tail radius not matching\");        ",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket parachutes\", function () {",
-											"        pm.expect(apiRspn.rocket.parachutes.name).to.eql(pm.environment.get('parachutes_names'), \"rocket parachutes names not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.cd_s).to.eql(pm.environment.get('parachutes_cds'), \"rocket parachutes cd_s not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.sampling_rate).to.eql(pm.environment.get('parachutes_sampling_rate'), \"rocket parachutes sampling_rate not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.lag).to.eql(pm.environment.get('parachutes_lags'), \"rocket parachutes lags not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.noise).to.eql(pm.environment.get('parachutes_noises'), \"rocket parachutes noises not matching\");",
-											"        pm.expect(apiRspn.rocket.parachutes.triggers).to.eql(pm.environment.get('parachutes_triggers'), \"rocket parachutes triggers not matching\");",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Read rocketpy Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid rocketpy Flight GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.jsonpickle_rocketpy_flight).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/rocketpy/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"rocketpy",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Simulate Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"//TEST",
-											"bdd = \"Given a valid rocketpy Flight simulate GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.flight_data).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_angular_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_angular_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.max_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.max_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.min_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.relative_error_tolerance).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.absolute_error_tolerance).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.time_overshoot).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.terminate_on_apogee).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.number_of_time_steps).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.function_evaluations_per_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.avg_function_evaluations_per_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.rail_length).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.flight_inclination).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.flight_heading).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions.frontal_surface_wind_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions.lateral_surface_wind_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_static_margin).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_angle_of_attack).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_thrust_weight_ratio).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_reynolds_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_rocket_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_freestream_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_mach_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_kinetic_energy).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_freestream_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_mach_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_reynolds_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_dynamic_pressure).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_acceleration_during_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_acceleration_after_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_gs_during_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_gs_after_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_upper_rail_button_normal_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_upper_rail_button_shear_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_lower_rail_button_normal_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_lower_rail_button_shear_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.x_impact_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.y_impact_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.time_of_impact).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.impact_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace.Drogue).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace.Main).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/simulate",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"simulate"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// reduce environment date for future assertion",
-											"flightRequest.environment.date = flightRequest.environment.date.substring(0, flightRequest.environment.date.length - 7);",
-											"",
-											"// save flight parameters",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"pm.environment.set('rail_length', flightRequest.rail_length)        ",
-											"pm.environment.set('inclination', flightRequest.inclination)",
-											"pm.environment.set('heading', flightRequest.heading)",
-											"",
-											"// flight environment",
-											"pm.environment.set('latitude', flightRequest.environment.latitude)",
-											"pm.environment.set('longitude', flightRequest.environment.longitude)",
-											"pm.environment.set('elevation', flightRequest.environment.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.environment.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.environment.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.environment.date)        ",
-											"",
-											"// flight rocket",
-											"pm.environment.set('radius', flightRequest.rocket.radius)",
-											"pm.environment.set('mass', flightRequest.rocket.mass)",
-											"pm.environment.set('inertia', flightRequest.rocket.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.rocket.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.rocket.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.rocket.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.rocket.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rocket.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rocket.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rocket.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rocket.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.rocket.coordinate_system_orientation)",
-											"",
-											"// flight rocket motor",
-											"pm.environment.set('burn_time', flightRequest.rocket.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.rocket.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.rocket.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.rocket.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.rocket.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.rocket.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.rocket.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.rocket.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.rocket.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.rocket.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.rocket.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.rocket.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.rocket.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.rocket.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.rocket.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.rocket.motor.coordinate_system_orientation)",
-											"",
-											"// flight rocket nose",
-											"pm.environment.set('nose_length', flightRequest.rocket.nose.length)",
-											"pm.environment.set('kind', flightRequest.rocket.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.rocket.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.rocket.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.rocket.nose.rocket_radius)",
-											"",
-											"// flight rocket fins",
-											"pm.environment.set('n', flightRequest.rocket.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.rocket.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.rocket.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.rocket.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.rocket.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.rocket.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.rocket.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.rocket.fins.airfoil)",
-											"",
-											"// flight rocket tail",
-											"pm.environment.set('top_radius', flightRequest.rocket.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.rocket.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.rocket.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.rocket.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.rocket.tail.radius)",
-											"",
-											"// flight rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.rocket.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.rocket.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.rocket.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.rocket.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.rocket.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.rocket.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"environment\": {\n    \"atmospheric_model_file\": \"GFS\",\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"date\": \"2023-12-29T10:22:00.921396\",\n    \"elevation\": 1300,\n    \"latitude\": 2,\n    \"longitude\": 1\n  },\n  \"rocket\": {\n    \"center_of_mass_without_motor\": 0,\n    \"coordinate_system_orientation\": \"tail_to_nose\",\n    \"fins\": {\n      \"airfoil\": \"\",\n      \"cant_angle\": 0,\n      \"n\": 4,\n      \"position\": -1.04956,\n      \"radius\": 0.0635,\n      \"root_chord\": 0.12,\n      \"span\": 0.1,\n      \"tip_chord\": 0.04\n    },\n    \"inertia\": [\n      6.321,\n      6.321,\n      0.0346\n    ],\n    \"mass\": 16.235,\n    \"motor\": {\n      \"burn_time\": 3.9,\n      \"center_of_dry_mass_position\": 0.317,\n      \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n      \"dry_inertia\": [\n        0.125,\n        0.125,\n        0.002\n      ],\n      \"dry_mass\": 1.815,\n      \"grain_density\": 1815,\n      \"grain_initial_height\": 0.12,\n      \"grain_initial_inner_radius\": 0.015,\n      \"grain_number\": 5,\n      \"grain_outer_radius\": 0.033,\n      \"grain_separation\": 0.005,\n      \"grains_center_of_mass_position\": -0.85704,\n      \"interpolation_method\": \"linear\",\n      \"nozzle_radius\": 0.033,\n      \"tanks\": [\n        {\n          \"discretize\": 100,\n          \"flux_time\": [\n            0,\n            8\n          ],\n          \"gas\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"gas_mass\": 0.1,\n          \"gas_mass_flow_rate_in\": 0.1,\n          \"gas_mass_flow_rate_out\": 0.1,\n          \"geometry\": [\n            [\n              [\n                0,\n                5\n              ],\n              1\n            ],\n            [\n              [\n                5,\n                10\n              ],\n              2\n            ]\n          ],\n          \"initial_gas_mass\": 0.1,\n          \"initial_liquid_mass\": 5,\n          \"liquid\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"liquid_height\": 0.5,\n          \"liquid_mass\": 5,\n          \"liquid_mass_flow_rate_in\": 0.1,\n          \"liquid_mass_flow_rate_out\": 0.1,\n          \"name\": \"Tank\",\n          \"position\": 1,\n          \"tank_kind\": \"MassFlow\",\n          \"ullage\": 0.1\n        }\n      ],\n      \"throat_radius\": 0.011,\n      \"thrust_source\": \"Cesaroni_M1670\"\n    },\n    \"motor_position\": -1.255,\n    \"nose\": {\n      \"base_radius\": 0.0635,\n      \"kind\": \"vonKarman\",\n      \"length\": 0.55829,\n      \"position\": 1.278,\n      \"rocket_radius\": 0.0635\n    },\n    \"parachutes\": {\n      \"cd_s\": [\n        10,\n        1\n      ],\n      \"lag\": [\n        1.5,\n        1.5\n      ],\n      \"name\": [\n        \"Main\",\n        \"Drogue\"\n      ],\n      \"noise\": [\n        [\n          0,\n          8.3,\n          0.5\n        ],\n        [\n          0,\n          8.3,\n          0.5\n        ]\n      ],\n      \"sampling_rate\": [\n        105,\n        105\n      ],\n      \"triggers\": [\n        \"lambda p, h, y: y[5] < 0 and h < 800\",\n        \"lambda p, h, y: y[5] < 0\"\n      ]\n    },\n    \"power_off_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"power_on_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"radius\": 0.0632,\n    \"rail_buttons\": {\n      \"angular_position\": 45,\n      \"lower_button_position\": 0.2,\n      \"upper_button_position\": -0.5\n    },\n    \"tail\": {\n      \"bottom_radius\": 0.0435,\n      \"length\": 0.06,\n      \"position\": -1.194656,\n      \"radius\": 0.0635,\n      \"top_radius\": 0.0635\n    }\n  },\n  \"inclination\": 85,\n  \"heading\": 0,\n  \"rail_length\": 5.2\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/?rocket_option=Calisto&motor_kind=Hybrid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										""
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Hybrid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight Environment",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// save new flight id",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"",
-											"// save environment parameters",
-											"pm.environment.set('env_id', apiRspn.new_env_id)        ",
-											"pm.environment.set('latitude', flightRequest.latitude)",
-											"pm.environment.set('longitude', flightRequest.longitude)",
-											"pm.environment.set('elevation', flightRequest.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.date)    ",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n    \"latitude\": 0,\n    \"longitude\": 0,\n    \"elevation\": 1400,\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"atmospheric_model_file\": \"GFS\",\n    \"date\": \"2023-05-09T16:30:50.065992\"\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/env",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"env"
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight Rocket",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// save new flight id",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"",
-											"// save rocket parameters",
-											"pm.environment.set('rocket_id', apiRspn.new_rocket_id)",
-											"pm.environment.set('radius', flightRequest.radius)",
-											"pm.environment.set('mass', flightRequest.mass)",
-											"pm.environment.set('inertia', flightRequest.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.coordinate_system_orientation)",
-											"",
-											"// rocket motor",
-											"pm.environment.set('burn_time', flightRequest.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.motor.coordinate_system_orientation)",
-											"",
-											"// rocket nose",
-											"pm.environment.set('nose_length', flightRequest.nose.length)",
-											"pm.environment.set('kind', flightRequest.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.nose.rocket_radius)",
-											"",
-											"// rocket fins",
-											"pm.environment.set('n', flightRequest.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.fins.airfoil)",
-											"",
-											"// rocket tail",
-											"pm.environment.set('top_radius', flightRequest.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.tail.radius)",
-											"",
-											"// rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"rail_buttons\": {\n    \"angular_position\": 45,\n    \"lower_button_position\": 0.2,\n    \"upper_button_position\": -0.5\n  },\n  \"motor\": {\n    \"burn_time\": 6.8,\n    \"center_of_dry_mass_position\": 0.512,\n    \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n    \"dry_inertia\": [\n      0.125,\n      0.125,\n      0.002\n    ],\n    \"dry_mass\": 1.815,\n    \"grain_density\": 1815,\n    \"grain_initial_height\": 0.12,\n    \"grain_initial_inner_radius\": 0.015,\n    \"grain_number\": 5,\n    \"grain_outer_radius\": 0.033,\n    \"grain_separation\": 0.005,\n    \"grains_center_of_mass_position\": -0.85704,\n    \"interpolation_method\": \"linear\",\n    \"nozzle_radius\": 0.033,\n    \"tanks\": [\n      {\n        \"discretize\": 100,\n        \"flux_time\": [\n          0,\n          8\n        ],\n        \"gas\": {\n          \"density\": 100,\n          \"name\": \"FluidName\"\n        },\n        \"gas_mass\": 0.1,\n        \"gas_mass_flow_rate_in\": 0.1,\n        \"gas_mass_flow_rate_out\": 0.1,\n        \"geometry\": [\n          [\n            [\n              0,\n              5\n            ],\n            1\n          ],\n          [\n            [\n              5,\n              10\n            ],\n            2\n          ]\n        ],\n        \"initial_gas_mass\": 0.1,\n        \"initial_liquid_mass\": 10,\n        \"liquid\": {\n          \"density\": 10,\n          \"name\": \"FluidName\"\n        },\n        \"liquid_height\": 0.5,\n        \"liquid_mass\": 5,\n        \"liquid_mass_flow_rate_in\": 0.1,\n        \"liquid_mass_flow_rate_out\": 0.1,\n        \"name\": \"Tank\",\n        \"position\": 1,\n        \"tank_kind\": \"MassFlow\",\n        \"ullage\": 0.1\n      }\n    ],\n    \"throat_radius\": 0.011,\n    \"thrust_source\": \"Cesaroni_M1670\"\n  },\n  \"nose\": {\n    \"base_radius\": 0.0635,\n    \"kind\": \"vonKarman\",\n    \"length\": 0.55829,\n    \"position\": 1.278,\n    \"rocket_radius\": 0.0635\n  },\n  \"fins\": {\n    \"airfoil\": \"\",\n    \"cant_angle\": 0,\n    \"n\": 4,\n    \"position\": -1.04956,\n    \"radius\": 0.0635,\n    \"root_chord\": 0.12,\n    \"span\": 0.1,\n    \"tip_chord\": 0.04\n  },\n  \"tail\": {\n    \"bottom_radius\": 0.0435,\n    \"length\": 0.06,\n    \"position\": -1.194656,\n    \"radius\": 0.0635,\n    \"top_radius\": 0.0635\n  },\n  \"parachutes\": {\n    \"cd_s\": [\n      10,\n      1\n    ],\n    \"lag\": [\n      1.5,\n      1.5\n    ],\n    \"name\": [\n      \"Main\",\n      \"Drogue\"\n    ],\n    \"noise\": [\n      [\n        0,\n        8.3,\n        0.5\n      ],\n      [\n        0,\n        8.3,\n        0.5\n      ]\n    ],\n    \"sampling_rate\": [\n      105,\n      105\n    ],\n    \"triggers\": [\n      \"lambda p, h, y: y[5] < 0 and h < 800\",\n      \"lambda p, h, y: y[5] < 0\"\n    ]\n  },\n  \"inertia\": [\n    6.321,\n    6.321,\n    0.0346\n  ],\n  \"center_of_mass_without_motor\": 0,\n  \"radius\": 0.0632,\n  \"mass\": 16.235,\n  \"motor_position\": -1.255,\n  \"power_off_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"power_on_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"coordinate_system_orientation\": \"tail_to_nose\"\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/rocket?rocket_option=Calisto&motor_kind=Hybrid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"rocket"
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Hybrid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Delete Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"//TEST",
-											"bdd = \"Given a valid Flight DELETE request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully deleted\", \"message not matching\");",
-											"        pm.expect(apiRspn.deleted_flight_id).to.eql(pm.environment.get('flight_id'), \"flight_id not matching\");                ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "DELETE",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						}
-					]
-				},
-				{
-					"name": "Liquid",
-					"item": [
-						{
-							"name": "Create Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// reduce environment date for future assertion",
-											"flightRequest.environment.date = flightRequest.environment.date.substring(0, flightRequest.environment.date.length - 7);",
-											"",
-											"// save flight parameters",
-											"pm.environment.set('rail_length', flightRequest.rail_length)        ",
-											"pm.environment.set('inclination', flightRequest.inclination)",
-											"pm.environment.set('heading', flightRequest.heading)",
-											"",
-											"// flight environment",
-											"pm.environment.set('flight_id', apiRspn.flight_id)        ",
-											"pm.environment.set('latitude', flightRequest.environment.latitude)",
-											"pm.environment.set('longitude', flightRequest.environment.longitude)",
-											"pm.environment.set('elevation', flightRequest.environment.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.environment.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.environment.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.environment.date)        ",
-											"",
-											"// flight rocket",
-											"pm.environment.set('radius', flightRequest.rocket.radius)",
-											"pm.environment.set('mass', flightRequest.rocket.mass)",
-											"pm.environment.set('inertia', flightRequest.rocket.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.rocket.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.rocket.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.rocket.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.rocket.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rocket.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rocket.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rocket.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rocket.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.rocket.coordinate_system_orientation)",
-											"",
-											"// flight rocket motor",
-											"pm.environment.set('burn_time', flightRequest.rocket.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.rocket.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.rocket.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.rocket.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.rocket.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.rocket.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.rocket.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.rocket.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.rocket.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.rocket.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.rocket.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.rocket.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.rocket.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.rocket.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.rocket.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.rocket.motor.coordinate_system_orientation)",
-											"",
-											"// flight rocket nose",
-											"pm.environment.set('nose_length', flightRequest.rocket.nose.length)",
-											"pm.environment.set('kind', flightRequest.rocket.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.rocket.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.rocket.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.rocket.nose.rocket_radius)",
-											"",
-											"// flight rocket fins",
-											"pm.environment.set('n', flightRequest.rocket.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.rocket.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.rocket.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.rocket.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.rocket.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.rocket.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.rocket.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.rocket.fins.airfoil)",
-											"",
-											"// flight rocket tail",
-											"pm.environment.set('top_radius', flightRequest.rocket.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.rocket.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.rocket.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.rocket.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.rocket.tail.radius)",
-											"",
-											"// flight rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.rocket.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.rocket.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.rocket.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.rocket.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.rocket.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.rocket.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight POST request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully created\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight_id\", function () {",
-											"        pm.expect(apiRspn.flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "POST",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"environment\": {\n    \"atmospheric_model_file\": \"GFS\",\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"date\": \"2023-12-29T10:22:00.921396\",\n    \"elevation\": 1400,\n    \"latitude\": 0,\n    \"longitude\": 0\n  },\n  \"rocket\": {\n    \"center_of_mass_without_motor\": 0,\n    \"coordinate_system_orientation\": \"tail_to_nose\",\n    \"fins\": {\n      \"airfoil\": \"\",\n      \"cant_angle\": 0,\n      \"n\": 4,\n      \"position\": -1.04956,\n      \"radius\": 0.0635,\n      \"root_chord\": 0.12,\n      \"span\": 0.1,\n      \"tip_chord\": 0.04\n    },\n    \"inertia\": [\n      6.321,\n      6.321,\n      0.0346\n    ],\n    \"mass\": 16.235,\n    \"motor\": {\n      \"burn_time\": 3.9,\n      \"center_of_dry_mass_position\": 0.317,\n      \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n      \"dry_inertia\": [\n        0.125,\n        0.125,\n        0.002\n      ],\n      \"dry_mass\": 1.815,\n      \"grain_density\": 1815,\n      \"grain_initial_height\": 0.12,\n      \"grain_initial_inner_radius\": 0.015,\n      \"grain_number\": 5,\n      \"grain_outer_radius\": 0.033,\n      \"grain_separation\": 0.005,\n      \"grains_center_of_mass_position\": -0.85704,\n      \"interpolation_method\": \"linear\",\n      \"nozzle_radius\": 0.033,\n      \"tanks\": [\n        {\n          \"discretize\": 100,\n          \"flux_time\": [\n            0,\n            8\n          ],\n          \"gas\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"gas_mass\": 0.1,\n          \"gas_mass_flow_rate_in\": 0.1,\n          \"gas_mass_flow_rate_out\": 0.1,\n          \"geometry\": [\n            [\n              [\n                0,\n                5\n              ],\n              1\n            ],\n            [\n              [\n                5,\n                10\n              ],\n              2\n            ]\n          ],\n          \"initial_gas_mass\": 0.1,\n          \"initial_liquid_mass\": 5,\n          \"liquid\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"liquid_height\": 0.5,\n          \"liquid_mass\": 5,\n          \"liquid_mass_flow_rate_in\": 0.1,\n          \"liquid_mass_flow_rate_out\": 0.1,\n          \"name\": \"Tank\",\n          \"position\": 1,\n          \"tank_kind\": \"MassFlow\",\n          \"ullage\": 0.1\n        }\n      ],\n      \"throat_radius\": 0.011,\n      \"thrust_source\": \"Cesaroni_M1670\"\n    },\n    \"motor_position\": -1.255,\n    \"nose\": {\n      \"base_radius\": 0.0635,\n      \"kind\": \"vonKarman\",\n      \"length\": 0.55829,\n      \"position\": 1.278,\n      \"rocket_radius\": 0.0635\n    },\n    \"parachutes\": {\n      \"cd_s\": [\n        10,\n        1\n      ],\n      \"lag\": [\n        1.5,\n        1.5\n      ],\n      \"name\": [\n        \"Main\",\n        \"Drogue\"\n      ],\n      \"noise\": [\n        [\n          0,\n          8.3,\n          0.5\n        ],\n        [\n          0,\n          8.3,\n          0.5\n        ]\n      ],\n      \"sampling_rate\": [\n        105,\n        105\n      ],\n      \"triggers\": [\n        \"lambda p, h, y: y[5] < 0 and h < 800\",\n        \"lambda p, h, y: y[5] < 0\"\n      ]\n    },\n    \"power_off_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"power_on_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"radius\": 0.0632,\n    \"rail_buttons\": {\n      \"angular_position\": 45,\n      \"lower_button_position\": 0.2,\n      \"upper_button_position\": -0.5\n    },\n    \"tail\": {\n      \"bottom_radius\": 0.0435,\n      \"length\": 0.06,\n      \"position\": -1.194656,\n      \"radius\": 0.0635,\n      \"top_radius\": 0.0635\n    }\n  },\n  \"inclination\": 85,\n  \"heading\": 0,\n  \"rail_length\": 5.2\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/?rocket_option=Calisto&motor_kind=Liquid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										""
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Liquid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Read Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"",
-											"var returned_date = apiRspn.environment.date;",
-											"var reduced_returned_date = returned_date.substring(0, returned_date.length - 7);",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight \", function () {",
-											"        pm.expect(apiRspn.inclination).to.eql(pm.environment.get('inclination'), \"flight inclination not matching\");",
-											"        pm.expect(apiRspn.heading).to.eql(pm.environment.get('heading'), \"flight heading not matching\");",
-											"        pm.expect(apiRspn.rail_length).to.eql(pm.environment.get('rail_length'), \"flight rail_length not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight environment\", function () {",
-											"        pm.expect(apiRspn.environment.longitude).to.eql(pm.environment.get('longitude'), \"environment longitude not matching\");        ",
-											"        pm.expect(apiRspn.environment.elevation).to.eql(pm.environment.get('elevation'), \"environment elevation not matching\");",
-											"        pm.expect(apiRspn.environment.atmospheric_model_type).to.eql(pm.environment.get('atmospheric_model_type'), \"environment atmospheric_model_type not matching\");",
-											"        pm.expect(apiRspn.environment.atmospheric_model_file).to.eql(pm.environment.get('atmospheric_model_file'), \"environment atmospheric_model_file not matching\");",
-											"        pm.expect(reduced_returned_date).to.eql(pm.environment.get('date'), \"date not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket\", function () {        ",
-											"        pm.expect(apiRspn.rocket.radius).to.eql(pm.environment.get('radius'), \"rocket radius not matching\");",
-											"        pm.expect(apiRspn.rocket.mass).to.eql(pm.environment.get('mass'), \"rocket mass not matching\");",
-											"        pm.expect(apiRspn.rocket.inertia).to.eql(pm.environment.get('inertia'), \"rocket inertia not matching\");",
-											"        pm.expect(apiRspn.rocket.power_off_drag).to.eql(pm.environment.get('power_off_drag'), \"rocket power_off_drag not matching\");",
-											"        pm.expect(apiRspn.rocket.power_on_drag).to.eql(pm.environment.get('power_on_drag'), \"rocket power_on_drag not matching\");",
-											"        pm.expect(apiRspn.rocket.center_of_mass_without_motor).to.eql(pm.environment.get('center_of_mass_without_motor'), \"rocket center_of_mass_without_motor not matching\");",
-											"        pm.expect(apiRspn.rocket.coordinate_system_orientation).to.eql(pm.environment.get('rocket_coordinate_system_orientation'), \"rocket coordinate_system_orientation not matching\");",
-											"        pm.expect(apiRspn.rocket.motor_position).to.eql(pm.environment.get('motor_position'), \"rocket motor_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons).to.eql(pm.environment.get('rail_buttons'), \"rocket rail_buttons not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.upper_button_position).to.eql(pm.environment.get('upper_button_position'), \"rocket rail_buttons upper_button_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.lower_button_position).to.eql(pm.environment.get('lower_button_position'), \"rocket rail_buttons lower_button_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.angular_position).to.eql(pm.environment.get('angular_position'), \"rocket rail_buttons angular_position not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket motor\", function () {",
-											"        pm.expect(apiRspn.rocket.motor.burn_time).to.eql(pm.environment.get('burn_time'), \"rocket motor burn_time not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.dry_mass).to.eql(pm.environment.get('dry_mass'), \"rocket motor dry_mass not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.dry_inertia).to.eql(pm.environment.get('dry_inertia'), \"rocket motor dry_inertia not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.center_of_dry_mass_position).to.eql(pm.environment.get('center_of_dry_mass_position'), \"rocket motor center_of_dry_mass_position not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_number).to.eql(pm.environment.get('grain_number'), \"rocket motor grain_number not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_density).to.eql(pm.environment.get('grain_density'), \"rocket motor grain_density not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_outer_radius).to.eql(pm.environment.get('grain_outer_radius'), \"rocket motor grain_outer_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_initial_inner_radius).to.eql(pm.environment.get('grain_initial_inner_radius'), \"rocket motor grain_initial_inner_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_initial_height).to.eql(pm.environment.get('grain_initial_height'), \"rocket motor grain_initial_height not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grains_center_of_mass_position).to.eql(pm.environment.get('grains_center_of_mass_position'), \"rocket motor grains_center_of_mass_position not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.thrust_source).to.eql(pm.environment.get('thrust_source'), \"rocket motor thrust_source not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_separation).to.eql(pm.environment.get('grain_separation'), \"rocket motor grain_separation not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.nozzle_radius).to.eql(pm.environment.get('nozzle_radius'), \"rocket motor nozzle_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.throat_radius).to.eql(pm.environment.get('throat_radius'), \"rocket motor throat_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.interpolation_method).to.eql(pm.environment.get('interpolation_method'), \"rocket motor interpolation_method not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.coordinate_system_orientation).to.eql(pm.environment.get('motor_coordinate_system_orientation'), \"motor coordinate_system_orientation not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket nose\", function () {",
-											"        pm.expect(apiRspn.rocket.nose.length).to.eql(pm.environment.get('nose_length'), \"rocket nose length not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.kind).to.eql(pm.environment.get('kind'), \"rocket nose kind not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.position).to.eql(pm.environment.get('nose_position'), \"rocket nose position not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.base_radius).to.eql(pm.environment.get('base_radius'), \"rocket nose base_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.rocket_radius).to.eql(pm.environment.get('rocket_radius'), \"rocket nose rocket_radius not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket fins\", function () {",
-											"        pm.expect(apiRspn.rocket.fins.n).to.eql(pm.environment.get('n'), \"rocket fins 'n' not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.root_chord).to.eql(pm.environment.get('root_chord'), \"rocket fins root_chord not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.tip_chord).to.eql(pm.environment.get('tip_chord'), \"rocket fins tip_chord not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.span).to.eql(pm.environment.get('span'), \"rocket fins span not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.position).to.eql(pm.environment.get('fin_position'), \"rocket fins position not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.cant_angle).to.eql(pm.environment.get('cant_angle'), \"rocket fins cant_angle not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.radius).to.eql(pm.environment.get('fin_radius'), \"rocket fins radius not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.airfoil).to.eql(pm.environment.get('airfoil'), \"rocket fins airfoil not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket tail\", function () {",
-											"        pm.expect(apiRspn.rocket.tail.top_radius).to.eql(pm.environment.get('top_radius'), \"rocket tail top_radius not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.bottom_radius).to.eql(pm.environment.get('bottom_radius'), \"rocket tail bottom_radius not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.length).to.eql(pm.environment.get('tail_length'), \"rocket tail length not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.position).to.eql(pm.environment.get('tail_position'), \"rocket tail position not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.radius).to.eql(pm.environment.get('tail_radius'), \"rocket tail radius not matching\");        ",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket parachutes\", function () {",
-											"        pm.expect(apiRspn.rocket.parachutes.name).to.eql(pm.environment.get('parachutes_names'), \"rocket parachutes names not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.cd_s).to.eql(pm.environment.get('parachutes_cds'), \"rocket parachutes cd_s not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.sampling_rate).to.eql(pm.environment.get('parachutes_sampling_rate'), \"rocket parachutes sampling_rate not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.lag).to.eql(pm.environment.get('parachutes_lags'), \"rocket parachutes lags not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.noise).to.eql(pm.environment.get('parachutes_noises'), \"rocket parachutes noises not matching\");",
-											"        pm.expect(apiRspn.rocket.parachutes.triggers).to.eql(pm.environment.get('parachutes_triggers'), \"rocket parachutes triggers not matching\");",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Read rocketpy Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid rocketpy Flight GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.jsonpickle_rocketpy_flight).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/rocketpy/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"rocketpy",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Simulate Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"//TEST",
-											"bdd = \"Given a valid rocketpy Flight simulate GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.flight_data).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_angular_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_angular_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.max_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.max_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.min_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.relative_error_tolerance).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.absolute_error_tolerance).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.time_overshoot).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.terminate_on_apogee).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.number_of_time_steps).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.function_evaluations_per_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.avg_function_evaluations_per_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.rail_length).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.flight_inclination).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.flight_heading).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions.frontal_surface_wind_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions.lateral_surface_wind_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_static_margin).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_angle_of_attack).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_thrust_weight_ratio).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_reynolds_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_rocket_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_freestream_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_mach_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_kinetic_energy).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_freestream_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_mach_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_reynolds_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_dynamic_pressure).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_acceleration_during_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_acceleration_after_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_gs_during_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_gs_after_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_upper_rail_button_normal_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_upper_rail_button_shear_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_lower_rail_button_normal_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_lower_rail_button_shear_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.x_impact_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.y_impact_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.time_of_impact).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.impact_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace.Drogue).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace.Main).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/simulate",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"simulate"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// reduce environment date for future assertion",
-											"flightRequest.environment.date = flightRequest.environment.date.substring(0, flightRequest.environment.date.length - 7);",
-											"",
-											"// save flight parameters",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"pm.environment.set('rail_length', flightRequest.rail_length)        ",
-											"pm.environment.set('inclination', flightRequest.inclination)",
-											"pm.environment.set('heading', flightRequest.heading)",
-											"",
-											"// flight environment",
-											"pm.environment.set('latitude', flightRequest.environment.latitude)",
-											"pm.environment.set('longitude', flightRequest.environment.longitude)",
-											"pm.environment.set('elevation', flightRequest.environment.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.environment.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.environment.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.environment.date)        ",
-											"",
-											"// flight rocket",
-											"pm.environment.set('radius', flightRequest.rocket.radius)",
-											"pm.environment.set('mass', flightRequest.rocket.mass)",
-											"pm.environment.set('inertia', flightRequest.rocket.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.rocket.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.rocket.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.rocket.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.rocket.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rocket.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rocket.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rocket.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rocket.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.rocket.coordinate_system_orientation)",
-											"",
-											"// flight rocket motor",
-											"pm.environment.set('burn_time', flightRequest.rocket.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.rocket.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.rocket.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.rocket.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.rocket.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.rocket.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.rocket.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.rocket.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.rocket.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.rocket.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.rocket.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.rocket.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.rocket.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.rocket.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.rocket.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.rocket.motor.coordinate_system_orientation)",
-											"",
-											"// flight rocket nose",
-											"pm.environment.set('nose_length', flightRequest.rocket.nose.length)",
-											"pm.environment.set('kind', flightRequest.rocket.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.rocket.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.rocket.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.rocket.nose.rocket_radius)",
-											"",
-											"// flight rocket fins",
-											"pm.environment.set('n', flightRequest.rocket.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.rocket.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.rocket.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.rocket.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.rocket.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.rocket.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.rocket.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.rocket.fins.airfoil)",
-											"",
-											"// flight rocket tail",
-											"pm.environment.set('top_radius', flightRequest.rocket.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.rocket.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.rocket.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.rocket.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.rocket.tail.radius)",
-											"",
-											"// flight rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.rocket.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.rocket.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.rocket.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.rocket.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.rocket.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.rocket.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"environment\": {\n    \"atmospheric_model_file\": \"GFS\",\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"date\": \"2023-12-29T10:22:00.921396\",\n    \"elevation\": 1300,\n    \"latitude\": 2,\n    \"longitude\": 1\n  },\n  \"rocket\": {\n    \"center_of_mass_without_motor\": 0,\n    \"coordinate_system_orientation\": \"tail_to_nose\",\n    \"fins\": {\n      \"airfoil\": \"\",\n      \"cant_angle\": 0,\n      \"n\": 4,\n      \"position\": -1.04956,\n      \"radius\": 0.0635,\n      \"root_chord\": 0.12,\n      \"span\": 0.1,\n      \"tip_chord\": 0.04\n    },\n    \"inertia\": [\n      6.321,\n      6.321,\n      0.0346\n    ],\n    \"mass\": 16.235,\n    \"motor\": {\n      \"burn_time\": 3.9,\n      \"center_of_dry_mass_position\": 0.317,\n      \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n      \"dry_inertia\": [\n        0.125,\n        0.125,\n        0.002\n      ],\n      \"dry_mass\": 1.815,\n      \"grain_density\": 1815,\n      \"grain_initial_height\": 0.12,\n      \"grain_initial_inner_radius\": 0.015,\n      \"grain_number\": 5,\n      \"grain_outer_radius\": 0.033,\n      \"grain_separation\": 0.005,\n      \"grains_center_of_mass_position\": -0.85704,\n      \"interpolation_method\": \"linear\",\n      \"nozzle_radius\": 0.033,\n      \"tanks\": [\n        {\n          \"discretize\": 100,\n          \"flux_time\": [\n            0,\n            8\n          ],\n          \"gas\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"gas_mass\": 0.1,\n          \"gas_mass_flow_rate_in\": 0.1,\n          \"gas_mass_flow_rate_out\": 0.1,\n          \"geometry\": [\n            [\n              [\n                0,\n                5\n              ],\n              1\n            ],\n            [\n              [\n                5,\n                10\n              ],\n              2\n            ]\n          ],\n          \"initial_gas_mass\": 0.1,\n          \"initial_liquid_mass\": 5,\n          \"liquid\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"liquid_height\": 0.5,\n          \"liquid_mass\": 5,\n          \"liquid_mass_flow_rate_in\": 0.1,\n          \"liquid_mass_flow_rate_out\": 0.1,\n          \"name\": \"Tank\",\n          \"position\": 1,\n          \"tank_kind\": \"MassFlow\",\n          \"ullage\": 0.1\n        }\n      ],\n      \"throat_radius\": 0.011,\n      \"thrust_source\": \"Cesaroni_M1670\"\n    },\n    \"motor_position\": -1.255,\n    \"nose\": {\n      \"base_radius\": 0.0635,\n      \"kind\": \"vonKarman\",\n      \"length\": 0.55829,\n      \"position\": 1.278,\n      \"rocket_radius\": 0.0635\n    },\n    \"parachutes\": {\n      \"cd_s\": [\n        10,\n        1\n      ],\n      \"lag\": [\n        1.5,\n        1.5\n      ],\n      \"name\": [\n        \"Main\",\n        \"Drogue\"\n      ],\n      \"noise\": [\n        [\n          0,\n          8.3,\n          0.5\n        ],\n        [\n          0,\n          8.3,\n          0.5\n        ]\n      ],\n      \"sampling_rate\": [\n        105,\n        105\n      ],\n      \"triggers\": [\n        \"lambda p, h, y: y[5] < 0 and h < 800\",\n        \"lambda p, h, y: y[5] < 0\"\n      ]\n    },\n    \"power_off_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"power_on_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"radius\": 0.0632,\n    \"rail_buttons\": {\n      \"angular_position\": 45,\n      \"lower_button_position\": 0.2,\n      \"upper_button_position\": -0.5\n    },\n    \"tail\": {\n      \"bottom_radius\": 0.0435,\n      \"length\": 0.06,\n      \"position\": -1.194656,\n      \"radius\": 0.0635,\n      \"top_radius\": 0.0635\n    }\n  },\n  \"inclination\": 85,\n  \"heading\": 0,\n  \"rail_length\": 5.2\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/?rocket_option=Calisto&motor_kind=Liquid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										""
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Liquid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight Environment",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// save new flight id",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"",
-											"// save environment parameters",
-											"pm.environment.set('env_id', apiRspn.new_env_id)        ",
-											"pm.environment.set('latitude', flightRequest.latitude)",
-											"pm.environment.set('longitude', flightRequest.longitude)",
-											"pm.environment.set('elevation', flightRequest.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.date)    ",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n    \"latitude\": 0,\n    \"longitude\": 0,\n    \"elevation\": 1400,\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"atmospheric_model_file\": \"GFS\",\n    \"date\": \"2023-05-09T16:30:50.065992\"\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/env",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"env"
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight Rocket",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// save new flight id",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"",
-											"// save rocket parameters",
-											"pm.environment.set('rocket_id', apiRspn.new_rocket_id)",
-											"pm.environment.set('radius', flightRequest.radius)",
-											"pm.environment.set('mass', flightRequest.mass)",
-											"pm.environment.set('inertia', flightRequest.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.coordinate_system_orientation)",
-											"",
-											"// rocket motor",
-											"pm.environment.set('burn_time', flightRequest.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.motor.coordinate_system_orientation)",
-											"",
-											"// rocket nose",
-											"pm.environment.set('nose_length', flightRequest.nose.length)",
-											"pm.environment.set('kind', flightRequest.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.nose.rocket_radius)",
-											"",
-											"// rocket fins",
-											"pm.environment.set('n', flightRequest.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.fins.airfoil)",
-											"",
-											"// rocket tail",
-											"pm.environment.set('top_radius', flightRequest.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.tail.radius)",
-											"",
-											"// rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"rail_buttons\": {\n    \"angular_position\": 45,\n    \"lower_button_position\": 0.2,\n    \"upper_button_position\": -0.5\n  },\n  \"motor\": {\n    \"burn_time\": 6.8,\n    \"center_of_dry_mass_position\": 0.512,\n    \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n    \"dry_inertia\": [\n      0.125,\n      0.125,\n      0.002\n    ],\n    \"dry_mass\": 1.815,\n    \"grain_density\": 1815,\n    \"grain_initial_height\": 0.12,\n    \"grain_initial_inner_radius\": 0.015,\n    \"grain_number\": 5,\n    \"grain_outer_radius\": 0.033,\n    \"grain_separation\": 0.005,\n    \"grains_center_of_mass_position\": -0.85704,\n    \"interpolation_method\": \"linear\",\n    \"nozzle_radius\": 0.033,\n    \"tanks\": [\n      {\n        \"discretize\": 100,\n        \"flux_time\": [\n          0,\n          8\n        ],\n        \"gas\": {\n          \"density\": 100,\n          \"name\": \"FluidName\"\n        },\n        \"gas_mass\": 0.1,\n        \"gas_mass_flow_rate_in\": 0.1,\n        \"gas_mass_flow_rate_out\": 0.1,\n        \"geometry\": [\n          [\n            [\n              0,\n              5\n            ],\n            1\n          ],\n          [\n            [\n              5,\n              10\n            ],\n            2\n          ]\n        ],\n        \"initial_gas_mass\": 0.1,\n        \"initial_liquid_mass\": 10,\n        \"liquid\": {\n          \"density\": 10,\n          \"name\": \"FluidName\"\n        },\n        \"liquid_height\": 0.5,\n        \"liquid_mass\": 5,\n        \"liquid_mass_flow_rate_in\": 0.1,\n        \"liquid_mass_flow_rate_out\": 0.1,\n        \"name\": \"Tank\",\n        \"position\": 1,\n        \"tank_kind\": \"MassFlow\",\n        \"ullage\": 0.1\n      }\n    ],\n    \"throat_radius\": 0.011,\n    \"thrust_source\": \"Cesaroni_M1670\"\n  },\n  \"nose\": {\n    \"base_radius\": 0.0635,\n    \"kind\": \"vonKarman\",\n    \"length\": 0.55829,\n    \"position\": 1.278,\n    \"rocket_radius\": 0.0635\n  },\n  \"fins\": {\n    \"airfoil\": \"\",\n    \"cant_angle\": 0,\n    \"n\": 4,\n    \"position\": -1.04956,\n    \"radius\": 0.0635,\n    \"root_chord\": 0.12,\n    \"span\": 0.1,\n    \"tip_chord\": 0.04\n  },\n  \"tail\": {\n    \"bottom_radius\": 0.0435,\n    \"length\": 0.06,\n    \"position\": -1.194656,\n    \"radius\": 0.0635,\n    \"top_radius\": 0.0635\n  },\n  \"parachutes\": {\n    \"cd_s\": [\n      10,\n      1\n    ],\n    \"lag\": [\n      1.5,\n      1.5\n    ],\n    \"name\": [\n      \"Main\",\n      \"Drogue\"\n    ],\n    \"noise\": [\n      [\n        0,\n        8.3,\n        0.5\n      ],\n      [\n        0,\n        8.3,\n        0.5\n      ]\n    ],\n    \"sampling_rate\": [\n      105,\n      105\n    ],\n    \"triggers\": [\n      \"lambda p, h, y: y[5] < 0 and h < 800\",\n      \"lambda p, h, y: y[5] < 0\"\n    ]\n  },\n  \"inertia\": [\n    6.321,\n    6.321,\n    0.0346\n  ],\n  \"center_of_mass_without_motor\": 0,\n  \"radius\": 0.0632,\n  \"mass\": 16.235,\n  \"motor_position\": -1.255,\n  \"power_off_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"power_on_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"coordinate_system_orientation\": \"tail_to_nose\"\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/rocket?rocket_option=Calisto&motor_kind=Liquid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"rocket"
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Liquid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Delete Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"//TEST",
-											"bdd = \"Given a valid Flight DELETE request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully deleted\", \"message not matching\");",
-											"        pm.expect(apiRspn.deleted_flight_id).to.eql(pm.environment.get('flight_id'), \"flight_id not matching\");                ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "DELETE",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						}
-					]
-				},
-				{
-					"name": "Solid",
-					"item": [
-						{
-							"name": "Create Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// reduce environment date for future assertion",
-											"flightRequest.environment.date = flightRequest.environment.date.substring(0, flightRequest.environment.date.length - 7);",
-											"",
-											"// save flight parameters",
-											"pm.environment.set('rail_length', flightRequest.rail_length)        ",
-											"pm.environment.set('inclination', flightRequest.inclination)",
-											"pm.environment.set('heading', flightRequest.heading)",
-											"",
-											"// flight environment",
-											"pm.environment.set('flight_id', apiRspn.flight_id)        ",
-											"pm.environment.set('latitude', flightRequest.environment.latitude)",
-											"pm.environment.set('longitude', flightRequest.environment.longitude)",
-											"pm.environment.set('elevation', flightRequest.environment.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.environment.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.environment.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.environment.date)        ",
-											"",
-											"// flight rocket",
-											"pm.environment.set('radius', flightRequest.rocket.radius)",
-											"pm.environment.set('mass', flightRequest.rocket.mass)",
-											"pm.environment.set('inertia', flightRequest.rocket.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.rocket.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.rocket.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.rocket.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.rocket.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rocket.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rocket.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rocket.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rocket.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.rocket.coordinate_system_orientation)",
-											"",
-											"// flight rocket motor",
-											"pm.environment.set('burn_time', flightRequest.rocket.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.rocket.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.rocket.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.rocket.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.rocket.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.rocket.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.rocket.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.rocket.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.rocket.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.rocket.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.rocket.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.rocket.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.rocket.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.rocket.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.rocket.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.rocket.motor.coordinate_system_orientation)",
-											"",
-											"// flight rocket nose",
-											"pm.environment.set('nose_length', flightRequest.rocket.nose.length)",
-											"pm.environment.set('kind', flightRequest.rocket.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.rocket.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.rocket.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.rocket.nose.rocket_radius)",
-											"",
-											"// flight rocket fins",
-											"pm.environment.set('n', flightRequest.rocket.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.rocket.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.rocket.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.rocket.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.rocket.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.rocket.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.rocket.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.rocket.fins.airfoil)",
-											"",
-											"// flight rocket tail",
-											"pm.environment.set('top_radius', flightRequest.rocket.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.rocket.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.rocket.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.rocket.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.rocket.tail.radius)",
-											"",
-											"// flight rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.rocket.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.rocket.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.rocket.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.rocket.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.rocket.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.rocket.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight POST request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully created\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight_id\", function () {",
-											"        pm.expect(apiRspn.flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "POST",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"environment\": {\n    \"atmospheric_model_file\": \"GFS\",\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"date\": \"2023-12-29T10:22:00.921396\",\n    \"elevation\": 1400,\n    \"latitude\": 0,\n    \"longitude\": 0\n  },\n  \"rocket\": {\n    \"center_of_mass_without_motor\": 0,\n    \"coordinate_system_orientation\": \"tail_to_nose\",\n    \"fins\": {\n      \"airfoil\": \"\",\n      \"cant_angle\": 0,\n      \"n\": 4,\n      \"position\": -1.04956,\n      \"radius\": 0.0635,\n      \"root_chord\": 0.12,\n      \"span\": 0.1,\n      \"tip_chord\": 0.04\n    },\n    \"inertia\": [\n      6.321,\n      6.321,\n      0.0346\n    ],\n    \"mass\": 16.235,\n    \"motor\": {\n      \"burn_time\": 3.9,\n      \"center_of_dry_mass_position\": 0.317,\n      \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n      \"dry_inertia\": [\n        0.125,\n        0.125,\n        0.002\n      ],\n      \"dry_mass\": 1.815,\n      \"grain_density\": 1815,\n      \"grain_initial_height\": 0.12,\n      \"grain_initial_inner_radius\": 0.015,\n      \"grain_number\": 5,\n      \"grain_outer_radius\": 0.033,\n      \"grain_separation\": 0.005,\n      \"grains_center_of_mass_position\": -0.85704,\n      \"interpolation_method\": \"linear\",\n      \"nozzle_radius\": 0.033,\n      \"tanks\": [\n        {\n          \"discretize\": 100,\n          \"flux_time\": [\n            0,\n            8\n          ],\n          \"gas\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"gas_mass\": 0.1,\n          \"gas_mass_flow_rate_in\": 0.1,\n          \"gas_mass_flow_rate_out\": 0.1,\n          \"geometry\": [\n            [\n              [\n                0,\n                5\n              ],\n              1\n            ],\n            [\n              [\n                5,\n                10\n              ],\n              2\n            ]\n          ],\n          \"initial_gas_mass\": 0.1,\n          \"initial_liquid_mass\": 5,\n          \"liquid\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"liquid_height\": 0.5,\n          \"liquid_mass\": 5,\n          \"liquid_mass_flow_rate_in\": 0.1,\n          \"liquid_mass_flow_rate_out\": 0.1,\n          \"name\": \"Tank\",\n          \"position\": 1,\n          \"tank_kind\": \"MassFlow\",\n          \"ullage\": 0.1\n        }\n      ],\n      \"throat_radius\": 0.011,\n      \"thrust_source\": \"Cesaroni_M1670\"\n    },\n    \"motor_position\": -1.255,\n    \"nose\": {\n      \"base_radius\": 0.0635,\n      \"kind\": \"vonKarman\",\n      \"length\": 0.55829,\n      \"position\": 1.278,\n      \"rocket_radius\": 0.0635\n    },\n    \"parachutes\": {\n      \"cd_s\": [\n        10,\n        1\n      ],\n      \"lag\": [\n        1.5,\n        1.5\n      ],\n      \"name\": [\n        \"Main\",\n        \"Drogue\"\n      ],\n      \"noise\": [\n        [\n          0,\n          8.3,\n          0.5\n        ],\n        [\n          0,\n          8.3,\n          0.5\n        ]\n      ],\n      \"sampling_rate\": [\n        105,\n        105\n      ],\n      \"triggers\": [\n        \"lambda p, h, y: y[5] < 0 and h < 800\",\n        \"lambda p, h, y: y[5] < 0\"\n      ]\n    },\n    \"power_off_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"power_on_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"radius\": 0.0632,\n    \"rail_buttons\": {\n      \"angular_position\": 45,\n      \"lower_button_position\": 0.2,\n      \"upper_button_position\": -0.5\n    },\n    \"tail\": {\n      \"bottom_radius\": 0.0435,\n      \"length\": 0.06,\n      \"position\": -1.194656,\n      \"radius\": 0.0635,\n      \"top_radius\": 0.0635\n    }\n  },\n  \"inclination\": 85,\n  \"heading\": 0,\n  \"rail_length\": 5.2\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/?rocket_option=Calisto&motor_kind=Solid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										""
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Solid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Read Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"",
-											"var returned_date = apiRspn.environment.date;",
-											"var reduced_returned_date = returned_date.substring(0, returned_date.length - 7);",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight \", function () {",
-											"        pm.expect(apiRspn.inclination).to.eql(pm.environment.get('inclination'), \"flight inclination not matching\");",
-											"        pm.expect(apiRspn.heading).to.eql(pm.environment.get('heading'), \"flight heading not matching\");",
-											"        pm.expect(apiRspn.rail_length).to.eql(pm.environment.get('rail_length'), \"flight rail_length not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight environment\", function () {",
-											"        pm.expect(apiRspn.environment.longitude).to.eql(pm.environment.get('longitude'), \"environment longitude not matching\");        ",
-											"        pm.expect(apiRspn.environment.elevation).to.eql(pm.environment.get('elevation'), \"environment elevation not matching\");",
-											"        pm.expect(apiRspn.environment.atmospheric_model_type).to.eql(pm.environment.get('atmospheric_model_type'), \"environment atmospheric_model_type not matching\");",
-											"        pm.expect(apiRspn.environment.atmospheric_model_file).to.eql(pm.environment.get('atmospheric_model_file'), \"environment atmospheric_model_file not matching\");",
-											"        pm.expect(reduced_returned_date).to.eql(pm.environment.get('date'), \"date not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket\", function () {        ",
-											"        pm.expect(apiRspn.rocket.radius).to.eql(pm.environment.get('radius'), \"rocket radius not matching\");",
-											"        pm.expect(apiRspn.rocket.mass).to.eql(pm.environment.get('mass'), \"rocket mass not matching\");",
-											"        pm.expect(apiRspn.rocket.inertia).to.eql(pm.environment.get('inertia'), \"rocket inertia not matching\");",
-											"        pm.expect(apiRspn.rocket.power_off_drag).to.eql(pm.environment.get('power_off_drag'), \"rocket power_off_drag not matching\");",
-											"        pm.expect(apiRspn.rocket.power_on_drag).to.eql(pm.environment.get('power_on_drag'), \"rocket power_on_drag not matching\");",
-											"        pm.expect(apiRspn.rocket.center_of_mass_without_motor).to.eql(pm.environment.get('center_of_mass_without_motor'), \"rocket center_of_mass_without_motor not matching\");",
-											"        pm.expect(apiRspn.rocket.coordinate_system_orientation).to.eql(pm.environment.get('rocket_coordinate_system_orientation'), \"rocket coordinate_system_orientation not matching\");",
-											"        pm.expect(apiRspn.rocket.motor_position).to.eql(pm.environment.get('motor_position'), \"rocket motor_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons).to.eql(pm.environment.get('rail_buttons'), \"rocket rail_buttons not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.upper_button_position).to.eql(pm.environment.get('upper_button_position'), \"rocket rail_buttons upper_button_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.lower_button_position).to.eql(pm.environment.get('lower_button_position'), \"rocket rail_buttons lower_button_position not matching\");",
-											"        pm.expect(apiRspn.rocket.rail_buttons.angular_position).to.eql(pm.environment.get('angular_position'), \"rocket rail_buttons angular_position not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket motor\", function () {",
-											"        pm.expect(apiRspn.rocket.motor.burn_time).to.eql(pm.environment.get('burn_time'), \"rocket motor burn_time not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.dry_mass).to.eql(pm.environment.get('dry_mass'), \"rocket motor dry_mass not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.dry_inertia).to.eql(pm.environment.get('dry_inertia'), \"rocket motor dry_inertia not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.center_of_dry_mass_position).to.eql(pm.environment.get('center_of_dry_mass_position'), \"rocket motor center_of_dry_mass_position not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_number).to.eql(pm.environment.get('grain_number'), \"rocket motor grain_number not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_density).to.eql(pm.environment.get('grain_density'), \"rocket motor grain_density not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_outer_radius).to.eql(pm.environment.get('grain_outer_radius'), \"rocket motor grain_outer_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_initial_inner_radius).to.eql(pm.environment.get('grain_initial_inner_radius'), \"rocket motor grain_initial_inner_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_initial_height).to.eql(pm.environment.get('grain_initial_height'), \"rocket motor grain_initial_height not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grains_center_of_mass_position).to.eql(pm.environment.get('grains_center_of_mass_position'), \"rocket motor grains_center_of_mass_position not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.thrust_source).to.eql(pm.environment.get('thrust_source'), \"rocket motor thrust_source not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.grain_separation).to.eql(pm.environment.get('grain_separation'), \"rocket motor grain_separation not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.nozzle_radius).to.eql(pm.environment.get('nozzle_radius'), \"rocket motor nozzle_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.throat_radius).to.eql(pm.environment.get('throat_radius'), \"rocket motor throat_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.interpolation_method).to.eql(pm.environment.get('interpolation_method'), \"rocket motor interpolation_method not matching\");",
-											"        pm.expect(apiRspn.rocket.motor.coordinate_system_orientation).to.eql(pm.environment.get('motor_coordinate_system_orientation'), \"motor coordinate_system_orientation not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket nose\", function () {",
-											"        pm.expect(apiRspn.rocket.nose.length).to.eql(pm.environment.get('nose_length'), \"rocket nose length not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.kind).to.eql(pm.environment.get('kind'), \"rocket nose kind not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.position).to.eql(pm.environment.get('nose_position'), \"rocket nose position not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.base_radius).to.eql(pm.environment.get('base_radius'), \"rocket nose base_radius not matching\");",
-											"        pm.expect(apiRspn.rocket.nose.rocket_radius).to.eql(pm.environment.get('rocket_radius'), \"rocket nose rocket_radius not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket fins\", function () {",
-											"        pm.expect(apiRspn.rocket.fins.n).to.eql(pm.environment.get('n'), \"rocket fins 'n' not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.root_chord).to.eql(pm.environment.get('root_chord'), \"rocket fins root_chord not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.tip_chord).to.eql(pm.environment.get('tip_chord'), \"rocket fins tip_chord not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.span).to.eql(pm.environment.get('span'), \"rocket fins span not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.position).to.eql(pm.environment.get('fin_position'), \"rocket fins position not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.cant_angle).to.eql(pm.environment.get('cant_angle'), \"rocket fins cant_angle not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.radius).to.eql(pm.environment.get('fin_radius'), \"rocket fins radius not matching\");",
-											"        pm.expect(apiRspn.rocket.fins.airfoil).to.eql(pm.environment.get('airfoil'), \"rocket fins airfoil not matching\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket tail\", function () {",
-											"        pm.expect(apiRspn.rocket.tail.top_radius).to.eql(pm.environment.get('top_radius'), \"rocket tail top_radius not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.bottom_radius).to.eql(pm.environment.get('bottom_radius'), \"rocket tail bottom_radius not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.length).to.eql(pm.environment.get('tail_length'), \"rocket tail length not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.position).to.eql(pm.environment.get('tail_position'), \"rocket tail position not matching\");        ",
-											"        pm.expect(apiRspn.rocket.tail.radius).to.eql(pm.environment.get('tail_radius'), \"rocket tail radius not matching\");        ",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid flight rocket parachutes\", function () {",
-											"        pm.expect(apiRspn.rocket.parachutes.name).to.eql(pm.environment.get('parachutes_names'), \"rocket parachutes names not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.cd_s).to.eql(pm.environment.get('parachutes_cds'), \"rocket parachutes cd_s not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.sampling_rate).to.eql(pm.environment.get('parachutes_sampling_rate'), \"rocket parachutes sampling_rate not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.lag).to.eql(pm.environment.get('parachutes_lags'), \"rocket parachutes lags not matching\");                ",
-											"        pm.expect(apiRspn.rocket.parachutes.noise).to.eql(pm.environment.get('parachutes_noises'), \"rocket parachutes noises not matching\");",
-											"        pm.expect(apiRspn.rocket.parachutes.triggers).to.eql(pm.environment.get('parachutes_triggers'), \"rocket parachutes triggers not matching\");",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Read rocketpy Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid rocketpy Flight GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.jsonpickle_rocketpy_flight).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/rocketpy/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"rocketpy",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Simulate Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"//TEST",
-											"bdd = \"Given a valid rocketpy Flight simulate GET request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.flight_data).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_angular_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.initial_conditions.initial_angular_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.max_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.max_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.min_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.relative_error_tolerance).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.absolute_error_tolerance).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.time_overshoot).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.terminate_on_apogee).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.number_of_time_steps).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.function_evaluations_per_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.numerical_integration_settings.avg_function_evaluations_per_time_step).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.rail_length).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.flight_inclination).to.exist;",
-											"        pm.expect(apiRspn.flight_data.launch_rail_conditions.flight_heading).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions.frontal_surface_wind_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.surface_wind_conditions.lateral_surface_wind_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_static_margin).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_angle_of_attack).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_thrust_weight_ratio).to.exist;",
-											"        pm.expect(apiRspn.flight_data.out_of_rail_conditions.out_of_rail_reynolds_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_rocket_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_freestream_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_mach_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.burnout_conditions.burnout_kinetic_energy).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_time).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_altitude).to.exist;",
-											"        pm.expect(apiRspn.flight_data.apogee_conditions.apogee_freestream_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_speed).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_mach_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_reynolds_number).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_dynamic_pressure).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_acceleration_during_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_acceleration_after_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_gs_during_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_gs_after_motor_burn).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_upper_rail_button_normal_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_upper_rail_button_shear_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_lower_rail_button_normal_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.maximum_values.maximum_lower_rail_button_shear_force).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.x_impact_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.y_impact_position).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.time_of_impact).to.exist;",
-											"        pm.expect(apiRspn.flight_data.impact_conditions.impact_velocity).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace.Drogue).to.exist;",
-											"        pm.expect(apiRspn.flight_data.events_registered.events_trace.Main).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "GET",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/simulate",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"simulate"
-									]
-								}
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// reduce environment date for future assertion",
-											"flightRequest.environment.date = flightRequest.environment.date.substring(0, flightRequest.environment.date.length - 7);",
-											"",
-											"// save flight parameters",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"pm.environment.set('rail_length', flightRequest.rail_length)        ",
-											"pm.environment.set('inclination', flightRequest.inclination)",
-											"pm.environment.set('heading', flightRequest.heading)",
-											"",
-											"// flight environment",
-											"pm.environment.set('latitude', flightRequest.environment.latitude)",
-											"pm.environment.set('longitude', flightRequest.environment.longitude)",
-											"pm.environment.set('elevation', flightRequest.environment.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.environment.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.environment.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.environment.date)        ",
-											"",
-											"// flight rocket",
-											"pm.environment.set('radius', flightRequest.rocket.radius)",
-											"pm.environment.set('mass', flightRequest.rocket.mass)",
-											"pm.environment.set('inertia', flightRequest.rocket.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.rocket.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.rocket.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.rocket.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.rocket.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rocket.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rocket.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rocket.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rocket.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.rocket.coordinate_system_orientation)",
-											"",
-											"// flight rocket motor",
-											"pm.environment.set('burn_time', flightRequest.rocket.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.rocket.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.rocket.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.rocket.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.rocket.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.rocket.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.rocket.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.rocket.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.rocket.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.rocket.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.rocket.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.rocket.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.rocket.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.rocket.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.rocket.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.rocket.motor.coordinate_system_orientation)",
-											"",
-											"// flight rocket nose",
-											"pm.environment.set('nose_length', flightRequest.rocket.nose.length)",
-											"pm.environment.set('kind', flightRequest.rocket.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.rocket.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.rocket.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.rocket.nose.rocket_radius)",
-											"",
-											"// flight rocket fins",
-											"pm.environment.set('n', flightRequest.rocket.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.rocket.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.rocket.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.rocket.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.rocket.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.rocket.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.rocket.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.rocket.fins.airfoil)",
-											"",
-											"// flight rocket tail",
-											"pm.environment.set('top_radius', flightRequest.rocket.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.rocket.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.rocket.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.rocket.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.rocket.tail.radius)",
-											"",
-											"// flight rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.rocket.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.rocket.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.rocket.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.rocket.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.rocket.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.rocket.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"environment\": {\n    \"atmospheric_model_file\": \"GFS\",\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"date\": \"2023-12-29T10:22:00.921396\",\n    \"elevation\": 1300,\n    \"latitude\": 2,\n    \"longitude\": 1\n  },\n  \"rocket\": {\n    \"center_of_mass_without_motor\": 0,\n    \"coordinate_system_orientation\": \"tail_to_nose\",\n    \"fins\": {\n      \"airfoil\": \"\",\n      \"cant_angle\": 0,\n      \"n\": 4,\n      \"position\": -1.04956,\n      \"radius\": 0.0635,\n      \"root_chord\": 0.12,\n      \"span\": 0.1,\n      \"tip_chord\": 0.04\n    },\n    \"inertia\": [\n      6.321,\n      6.321,\n      0.0346\n    ],\n    \"mass\": 16.235,\n    \"motor\": {\n      \"burn_time\": 3.9,\n      \"center_of_dry_mass_position\": 0.317,\n      \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n      \"dry_inertia\": [\n        0.125,\n        0.125,\n        0.002\n      ],\n      \"dry_mass\": 1.815,\n      \"grain_density\": 1815,\n      \"grain_initial_height\": 0.12,\n      \"grain_initial_inner_radius\": 0.015,\n      \"grain_number\": 5,\n      \"grain_outer_radius\": 0.033,\n      \"grain_separation\": 0.005,\n      \"grains_center_of_mass_position\": -0.85704,\n      \"interpolation_method\": \"linear\",\n      \"nozzle_radius\": 0.033,\n      \"tanks\": [\n        {\n          \"discretize\": 100,\n          \"flux_time\": [\n            0,\n            8\n          ],\n          \"gas\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"gas_mass\": 0.1,\n          \"gas_mass_flow_rate_in\": 0.1,\n          \"gas_mass_flow_rate_out\": 0.1,\n          \"geometry\": [\n            [\n              [\n                0,\n                5\n              ],\n              1\n            ],\n            [\n              [\n                5,\n                10\n              ],\n              2\n            ]\n          ],\n          \"initial_gas_mass\": 0.1,\n          \"initial_liquid_mass\": 5,\n          \"liquid\": {\n            \"density\": 100,\n            \"name\": \"FluidName\"\n          },\n          \"liquid_height\": 0.5,\n          \"liquid_mass\": 5,\n          \"liquid_mass_flow_rate_in\": 0.1,\n          \"liquid_mass_flow_rate_out\": 0.1,\n          \"name\": \"Tank\",\n          \"position\": 1,\n          \"tank_kind\": \"MassFlow\",\n          \"ullage\": 0.1\n        }\n      ],\n      \"throat_radius\": 0.011,\n      \"thrust_source\": \"Cesaroni_M1670\"\n    },\n    \"motor_position\": -1.255,\n    \"nose\": {\n      \"base_radius\": 0.0635,\n      \"kind\": \"vonKarman\",\n      \"length\": 0.55829,\n      \"position\": 1.278,\n      \"rocket_radius\": 0.0635\n    },\n    \"parachutes\": {\n      \"cd_s\": [\n        10,\n        1\n      ],\n      \"lag\": [\n        1.5,\n        1.5\n      ],\n      \"name\": [\n        \"Main\",\n        \"Drogue\"\n      ],\n      \"noise\": [\n        [\n          0,\n          8.3,\n          0.5\n        ],\n        [\n          0,\n          8.3,\n          0.5\n        ]\n      ],\n      \"sampling_rate\": [\n        105,\n        105\n      ],\n      \"triggers\": [\n        \"lambda p, h, y: y[5] < 0 and h < 800\",\n        \"lambda p, h, y: y[5] < 0\"\n      ]\n    },\n    \"power_off_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"power_on_drag\": [\n      [\n        0.01,\n        0.333865758\n      ],\n      [\n        0.02,\n        0.394981721\n      ],\n      [\n        0.03,\n        0.407756063\n      ]\n    ],\n    \"radius\": 0.0632,\n    \"rail_buttons\": {\n      \"angular_position\": 45,\n      \"lower_button_position\": 0.2,\n      \"upper_button_position\": -0.5\n    },\n    \"tail\": {\n      \"bottom_radius\": 0.0435,\n      \"length\": 0.06,\n      \"position\": -1.194656,\n      \"radius\": 0.0635,\n      \"top_radius\": 0.0635\n    }\n  },\n  \"inclination\": 85,\n  \"heading\": 0,\n  \"rail_length\": 5.2\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/?rocket_option=Calisto&motor_kind=Solid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										""
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Solid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight Environment",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// save new flight id",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"",
-											"// save environment parameters",
-											"pm.environment.set('env_id', apiRspn.new_env_id)        ",
-											"pm.environment.set('latitude', flightRequest.latitude)",
-											"pm.environment.set('longitude', flightRequest.longitude)",
-											"pm.environment.set('elevation', flightRequest.elevation)      ",
-											"pm.environment.set('atmospheric_model_type', flightRequest.atmospheric_model_type)    ",
-											"pm.environment.set('atmospheric_model_file', flightRequest.atmospheric_model_file)            ",
-											"pm.environment.set('date', flightRequest.date)    ",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n    \"latitude\": 0,\n    \"longitude\": 0,\n    \"elevation\": 1400,\n    \"atmospheric_model_type\": \"standard_atmosphere\",\n    \"atmospheric_model_file\": \"GFS\",\n    \"date\": \"2023-05-09T16:30:50.065992\"\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/env",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"env"
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Update Flight Rocket",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"var flightRequest = JSON.parse(pm.request.body.raw);",
-											"",
-											"// save new flight id",
-											"pm.environment.set('flight_id', apiRspn.new_flight_id)        ",
-											"",
-											"// save rocket parameters",
-											"pm.environment.set('rocket_id', apiRspn.new_rocket_id)",
-											"pm.environment.set('radius', flightRequest.radius)",
-											"pm.environment.set('mass', flightRequest.mass)",
-											"pm.environment.set('inertia', flightRequest.inertia)",
-											"pm.environment.set('power_off_drag', flightRequest.power_off_drag)",
-											"pm.environment.set('power_on_drag', flightRequest.power_on_drag)",
-											"pm.environment.set('center_of_mass_without_motor', flightRequest.center_of_mass_without_motor)",
-											"pm.environment.set('motor_position', flightRequest.motor_position)",
-											"pm.environment.set('rail_buttons', flightRequest.rail_buttons)",
-											"pm.environment.set('upper_button_position', flightRequest.rail_buttons.upper_button_position)",
-											"pm.environment.set('lower_button_position', flightRequest.rail_buttons.lower_button_position)",
-											"pm.environment.set('angular_position', flightRequest.rail_buttons.angular_position)",
-											"pm.environment.set('rocket_coordinate_system_orientation', flightRequest.coordinate_system_orientation)",
-											"",
-											"// rocket motor",
-											"pm.environment.set('burn_time', flightRequest.motor.burn_time)",
-											"pm.environment.set('dry_mass', flightRequest.motor.dry_mass)",
-											"pm.environment.set('dry_inertia', flightRequest.motor.dry_inertia)",
-											"pm.environment.set('center_of_dry_mass_position', flightRequest.motor.center_of_dry_mass_position)",
-											"pm.environment.set('grain_number', flightRequest.motor.grain_number)",
-											"pm.environment.set('grain_density', flightRequest.motor.grain_density)",
-											"pm.environment.set('grain_outer_radius', flightRequest.motor.grain_outer_radius)",
-											"pm.environment.set('grain_initial_inner_radius', flightRequest.motor.grain_initial_inner_radius)",
-											"pm.environment.set('grain_initial_height', flightRequest.motor.grain_initial_height)",
-											"pm.environment.set('grains_center_of_mass_position', flightRequest.motor.grains_center_of_mass_position)",
-											"pm.environment.set('grain_separation', flightRequest.motor.grain_separation)",
-											"pm.environment.set('thrust_source', flightRequest.motor.thrust_source)",
-											"pm.environment.set('nozzle_radius', flightRequest.motor.nozzle_radius)",
-											"pm.environment.set('throat_radius', flightRequest.motor.throat_radius)",
-											"pm.environment.set('interpolation_method', flightRequest.motor.interpolation_method)",
-											"pm.environment.set('motor_coordinate_system_orientation', flightRequest.motor.coordinate_system_orientation)",
-											"",
-											"// rocket nose",
-											"pm.environment.set('nose_length', flightRequest.nose.length)",
-											"pm.environment.set('kind', flightRequest.nose.kind)",
-											"pm.environment.set('nose_position', flightRequest.nose.position)",
-											"pm.environment.set('base_radius', flightRequest.nose.base_radius)",
-											"pm.environment.set('rocket_radius', flightRequest.nose.rocket_radius)",
-											"",
-											"// rocket fins",
-											"pm.environment.set('n', flightRequest.fins.n)",
-											"pm.environment.set('root_chord', flightRequest.fins.root_chord)",
-											"pm.environment.set('tip_chord', flightRequest.fins.tip_chord)",
-											"pm.environment.set('span', flightRequest.fins.span)",
-											"pm.environment.set('fin_position', flightRequest.fins.position)",
-											"pm.environment.set('cant_angle', flightRequest.fins.cant_angle)",
-											"pm.environment.set('fin_radius', flightRequest.fins.radius)",
-											"pm.environment.set('airfoil', flightRequest.fins.airfoil)",
-											"",
-											"// rocket tail",
-											"pm.environment.set('top_radius', flightRequest.tail.top_radius)",
-											"pm.environment.set('bottom_radius', flightRequest.tail.bottom_radius)",
-											"pm.environment.set('tail_length', flightRequest.tail.length)",
-											"pm.environment.set('tail_position', flightRequest.tail.position)",
-											"pm.environment.set('tail_radius', flightRequest.tail.radius)",
-											"",
-											"// rocket parachute",
-											"pm.environment.set('parachutes_names', flightRequest.parachutes.name)",
-											"pm.environment.set('parachutes_cds', flightRequest.parachutes.cd_s)",
-											"pm.environment.set('parachutes_sampling_rate', flightRequest.parachutes.sampling_rate)",
-											"pm.environment.set('parachutes_lags', flightRequest.parachutes.lag)",
-											"pm.environment.set('parachutes_noises', flightRequest.parachutes.noise)",
-											"pm.environment.set('parachutes_triggers', flightRequest.parachutes.triggers)",
-											"",
-											"//TEST",
-											"bdd = \"Given a valid Flight PUT request is made to the API\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully updated\");",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid new_flight_id\", function () {",
-											"        pm.expect(apiRspn.new_flight_id).to.exist;        ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								},
-								{
-									"listen": "prerequest",
-									"script": {
-										"exec": [
-											""
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "PUT",
-								"header": [],
-								"body": {
-									"mode": "raw",
-									"raw": "{\n  \"rail_buttons\": {\n    \"angular_position\": 45,\n    \"lower_button_position\": 0.2,\n    \"upper_button_position\": -0.5\n  },\n  \"motor\": {\n    \"burn_time\": 6.8,\n    \"center_of_dry_mass_position\": 0.512,\n    \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n    \"dry_inertia\": [\n      0.125,\n      0.125,\n      0.002\n    ],\n    \"dry_mass\": 1.815,\n    \"grain_density\": 1815,\n    \"grain_initial_height\": 0.12,\n    \"grain_initial_inner_radius\": 0.015,\n    \"grain_number\": 5,\n    \"grain_outer_radius\": 0.033,\n    \"grain_separation\": 0.005,\n    \"grains_center_of_mass_position\": -0.85704,\n    \"interpolation_method\": \"linear\",\n    \"nozzle_radius\": 0.033,\n    \"tanks\": [\n      {\n        \"discretize\": 100,\n        \"flux_time\": [\n          0,\n          8\n        ],\n        \"gas\": {\n          \"density\": 100,\n          \"name\": \"FluidName\"\n        },\n        \"gas_mass\": 0.1,\n        \"gas_mass_flow_rate_in\": 0.1,\n        \"gas_mass_flow_rate_out\": 0.1,\n        \"geometry\": [\n          [\n            [\n              0,\n              5\n            ],\n            1\n          ],\n          [\n            [\n              5,\n              10\n            ],\n            2\n          ]\n        ],\n        \"initial_gas_mass\": 0.1,\n        \"initial_liquid_mass\": 10,\n        \"liquid\": {\n          \"density\": 10,\n          \"name\": \"FluidName\"\n        },\n        \"liquid_height\": 0.5,\n        \"liquid_mass\": 5,\n        \"liquid_mass_flow_rate_in\": 0.1,\n        \"liquid_mass_flow_rate_out\": 0.1,\n        \"name\": \"Tank\",\n        \"position\": 1,\n        \"tank_kind\": \"MassFlow\",\n        \"ullage\": 0.1\n      }\n    ],\n    \"throat_radius\": 0.011,\n    \"thrust_source\": \"Cesaroni_M1670\"\n  },\n  \"nose\": {\n    \"base_radius\": 0.0635,\n    \"kind\": \"vonKarman\",\n    \"length\": 0.55829,\n    \"position\": 1.278,\n    \"rocket_radius\": 0.0635\n  },\n  \"fins\": {\n    \"airfoil\": \"\",\n    \"cant_angle\": 0,\n    \"n\": 4,\n    \"position\": -1.04956,\n    \"radius\": 0.0635,\n    \"root_chord\": 0.12,\n    \"span\": 0.1,\n    \"tip_chord\": 0.04\n  },\n  \"tail\": {\n    \"bottom_radius\": 0.0435,\n    \"length\": 0.06,\n    \"position\": -1.194656,\n    \"radius\": 0.0635,\n    \"top_radius\": 0.0635\n  },\n  \"parachutes\": {\n    \"cd_s\": [\n      10,\n      1\n    ],\n    \"lag\": [\n      1.5,\n      1.5\n    ],\n    \"name\": [\n      \"Main\",\n      \"Drogue\"\n    ],\n    \"noise\": [\n      [\n        0,\n        8.3,\n        0.5\n      ],\n      [\n        0,\n        8.3,\n        0.5\n      ]\n    ],\n    \"sampling_rate\": [\n      105,\n      105\n    ],\n    \"triggers\": [\n      \"lambda p, h, y: y[5] < 0 and h < 800\",\n      \"lambda p, h, y: y[5] < 0\"\n    ]\n  },\n  \"inertia\": [\n    6.321,\n    6.321,\n    0.0346\n  ],\n  \"center_of_mass_without_motor\": 0,\n  \"radius\": 0.0632,\n  \"mass\": 16.235,\n  \"motor_position\": -1.255,\n  \"power_off_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"power_on_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"coordinate_system_orientation\": \"tail_to_nose\"\n}",
-									"options": {
-										"raw": {
-											"language": "json"
-										}
-									}
-								},
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}/rocket?rocket_option=Calisto&motor_kind=Solid",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}",
-										"rocket"
-									],
-									"query": [
-										{
-											"key": "rocket_option",
-											"value": "Calisto"
-										},
-										{
-											"key": "motor_kind",
-											"value": "Solid"
-										}
-									]
-								},
-								"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-							},
-							"response": []
-						},
-						{
-							"name": "Delete Flight",
-							"event": [
-								{
-									"listen": "test",
-									"script": {
-										"exec": [
-											"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-											"if (responseCode.code == 500) {",
-											"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    return",
-											"}",
-											"",
-											"var apiRspn = pm.response.json();",
-											"//TEST",
-											"bdd = \"Given a valid Flight DELETE request is made\";",
-											"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-											"        pm.expect(responseCode.code).to.eql(200);",
-											"    });",
-											"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-											"        pm.expect(apiRspn.message).to.eql(\"Flight successfully deleted\", \"message not matching\");",
-											"        pm.expect(apiRspn.deleted_flight_id).to.eql(pm.environment.get('flight_id'), \"flight_id not matching\");                ",
-											"    });"
-										],
-										"type": "text/javascript"
-									}
-								}
-							],
-							"request": {
-								"method": "DELETE",
-								"header": [],
-								"url": {
-									"raw": "{{endpoint}}/flights/{{flight_id}}",
-									"host": [
-										"{{endpoint}}"
-									],
-									"path": [
-										"flights",
-										"{{flight_id}}"
-									]
-								}
-							},
-							"response": []
-						}
-					]
-				}
-			]
-		},
-		{
-			"name": "Motor",
-			"item": [
-				{
-					"name": "Create Motor",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"var motorRequest = JSON.parse(pm.request.body.raw);",
-									"",
-									"// save motor parameters",
-									"pm.environment.set('motor_id', apiRspn.motor_id)        ",
-									"pm.environment.set('burn_time', motorRequest.burn_time)",
-									"pm.environment.set('dry_mass', motorRequest.dry_mass)",
-									"pm.environment.set('dry_inertia', motorRequest.dry_inertia)",
-									"pm.environment.set('center_of_dry_mass_position', motorRequest.center_of_dry_mass_position)",
-									"pm.environment.set('grain_number', motorRequest.grain_number)",
-									"pm.environment.set('grain_density', motorRequest.grain_density)",
-									"pm.environment.set('grain_outer_radius', motorRequest.grain_outer_radius)",
-									"pm.environment.set('grain_initial_inner_radius', motorRequest.grain_initial_inner_radius)",
-									"pm.environment.set('grain_initial_height', motorRequest.grain_initial_height)",
-									"pm.environment.set('grains_center_of_mass_position', motorRequest.grains_center_of_mass_position)",
-									"pm.environment.set('grain_separation', motorRequest.grain_separation)",
-									"pm.environment.set('thrust_source', motorRequest.thrust_source)",
-									"pm.environment.set('nozzle_radius', motorRequest.nozzle_radius)",
-									"pm.environment.set('throat_radius', motorRequest.throat_radius)",
-									"pm.environment.set('interpolation_method', motorRequest.interpolation_method)",
-									"pm.environment.set('motor_coordinate_system_orientation', motorRequest.coordinate_system_orientation)",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Motor POST request is made to the API\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Motor successfully created\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid motor_id\", function () {",
-									"        pm.expect(apiRspn.motor_id).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						},
-						{
-							"listen": "prerequest",
-							"script": {
-								"exec": [
-									""
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "POST",
-						"header": [],
-						"body": {
-							"mode": "raw",
-							"raw": "{\n  \"thrust_source\": \"Cesaroni_M1670\",\n  \"burn_time\": 3.9,\n  \"nozzle_radius\": 0.033,\n  \"dry_mass\": 1.815,\n  \"dry_inertia\": [\n    0.125,\n    0.125,\n    0.002\n  ],\n  \"center_of_dry_mass_position\": 0.317,\n  \"tanks\": [\n    {\n      \"discretize\": 100,\n      \"flux_time\": [\n        0,\n        8\n      ],\n      \"gas\": {\n        \"density\": 100,\n        \"name\": \"FluidName\"\n      },\n      \"gas_mass\": 0.1,\n      \"gas_mass_flow_rate_in\": 0.1,\n      \"gas_mass_flow_rate_out\": 0.1,\n      \"geometry\": [\n        [\n          [\n            0,\n            5\n          ],\n          1\n        ],\n        [\n          [\n            5,\n            10\n          ],\n          2\n        ]\n      ],\n      \"initial_gas_mass\": 0.1,\n      \"initial_liquid_mass\": 5,\n      \"liquid\": {\n        \"density\": 100,\n        \"name\": \"FluidName\"\n      },\n      \"liquid_height\": 0.5,\n      \"liquid_mass\": 5,\n      \"liquid_mass_flow_rate_in\": 0.1,\n      \"liquid_mass_flow_rate_out\": 0.1,\n      \"name\": \"Tank\",\n      \"position\": 1,\n      \"tank_kind\": \"MassFlow\",\n      \"ullage\": 0.1\n    }\n  ],\n  \"grain_number\": 5,\n  \"grain_density\": 1815,\n  \"grain_outer_radius\": 0.033,\n  \"grain_initial_inner_radius\": 0.015,\n  \"grain_initial_height\": 0.12,\n  \"grains_center_of_mass_position\": -0.85704,\n  \"grain_separation\": 0.005,\n  \"throat_radius\": 0.011,\n  \"interpolation_method\": \"linear\",\n  \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\"\n}",
-							"options": {
-								"raw": {
-									"language": "json"
-								}
-							}
-						},
-						"url": {
-							"raw": "{{endpoint}}/motors/?motor_kind=Solid",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"motors",
-								""
-							],
-							"query": [
-								{
-									"key": "motor_kind",
-									"value": "Solid"
-								}
-							]
-						},
-						"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-					},
-					"response": []
-				},
-				{
-					"name": "Read Motor",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Motor GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });    ",
-									"    pm.test(bdd + \" then response must contain a valid motor\", function () {",
-									"        pm.expect(apiRspn.burn_time).to.eql(pm.environment.get('burn_time'), \"motor burn_time not matching\");",
-									"        pm.expect(apiRspn.dry_mass).to.eql(pm.environment.get('dry_mass'), \"motor dry_mass not matching\");",
-									"        pm.expect(apiRspn.dry_inertia).to.eql(pm.environment.get('dry_inertia'), \"motor dry_inertia not matching\");",
-									"        pm.expect(apiRspn.center_of_dry_mass_position).to.eql(pm.environment.get('center_of_dry_mass_position'), \"motor center_of_dry_mass_position not matching\");",
-									"        pm.expect(apiRspn.grain_number).to.eql(pm.environment.get('grain_number'), \"motor grain_number not matching\");",
-									"        pm.expect(apiRspn.grain_density).to.eql(pm.environment.get('grain_density'), \"motor grain_density not matching\");",
-									"        pm.expect(apiRspn.grain_outer_radius).to.eql(pm.environment.get('grain_outer_radius'), \"motor grain_outer_radius not matching\");",
-									"        pm.expect(apiRspn.grain_initial_inner_radius).to.eql(pm.environment.get('grain_initial_inner_radius'), \"motor grain_initial_inner_radius not matching\");",
-									"        pm.expect(apiRspn.grain_initial_height).to.eql(pm.environment.get('grain_initial_height'), \"motor grain_initial_height not matching\");",
-									"        pm.expect(apiRspn.grains_center_of_mass_position).to.eql(pm.environment.get('grains_center_of_mass_position'), \"motor grains_center_of_mass_position not matching\");",
-									"        pm.expect(apiRspn.thrust_source).to.eql(pm.environment.get('thrust_source'), \"motor thrust_source not matching\");",
-									"        pm.expect(apiRspn.grain_separation).to.eql(pm.environment.get('grain_separation'), \"motor grain_separation not matching\");",
-									"        pm.expect(apiRspn.nozzle_radius).to.eql(pm.environment.get('nozzle_radius'), \"motor nozzle_radius not matching\");",
-									"        pm.expect(apiRspn.throat_radius).to.eql(pm.environment.get('throat_radius'), \"motor throat_radius not matching\");",
-									"        pm.expect(apiRspn.interpolation_method).to.eql(pm.environment.get('interpolation_method'), \"motor interpolation_method not matching\");",
-									"        pm.expect(apiRspn.coordinate_system_orientation).to.eql(pm.environment.get('motor_coordinate_system_orientation'), \"motor coordinate_system_orientation not matching\");",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/motors/{{motor_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"motors",
-								"{{motor_id}}"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Read rocketpy Motor",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid rocketpy Motor GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.jsonpickle_rocketpy_motor).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/motors/rocketpy/{{motor_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"motors",
-								"rocketpy",
-								"{{motor_id}}"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Simulate Motor",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"//TEST",
-									"bdd = \"Given a valid rocketpy Motor simulate GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.motor_data).to.exist;",
-									"        pm.expect(apiRspn.motor_data.total_burning_time).to.exist;",
-									"        pm.expect(apiRspn.motor_data.total_propellant_mass).to.exist;",
-									"        pm.expect(apiRspn.motor_data.average_propellant_exhaust_velocity).to.exist;",
-									"        pm.expect(apiRspn.motor_data.average_thrust).to.exist;",
-									"        pm.expect(apiRspn.motor_data.maximum_thrust).to.exist;",
-									"        pm.expect(apiRspn.motor_data.total_impulse).to.exist;",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/motors/{{motor_id}}/simulate",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"motors",
-								"{{motor_id}}",
-								"simulate"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Update Motor",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"var motorRequest = JSON.parse(pm.request.body.raw);",
-									"",
-									"// save motor parameters",
-									"pm.environment.set('motor_id', apiRspn.new_motor_id)",
-									"pm.environment.set('burn_time', motorRequest.burn_time)",
-									"pm.environment.set('dry_mass', motorRequest.dry_mass)",
-									"pm.environment.set('dry_inertia', motorRequest.dry_inertia)",
-									"pm.environment.set('center_of_dry_mass_position', motorRequest.center_of_dry_mass_position)",
-									"pm.environment.set('grain_number', motorRequest.grain_number)",
-									"pm.environment.set('grain_density', motorRequest.grain_density)",
-									"pm.environment.set('grain_outer_radius', motorRequest.grain_outer_radius)",
-									"pm.environment.set('grain_initial_inner_radius', motorRequest.grain_initial_inner_radius)",
-									"pm.environment.set('grain_initial_height', motorRequest.grain_initial_height)",
-									"pm.environment.set('grains_center_of_mass_position', motorRequest.grains_center_of_mass_position)",
-									"pm.environment.set('grain_separation', motorRequest.grain_separation)",
-									"pm.environment.set('thrust_source', motorRequest.thrust_source)",
-									"pm.environment.set('nozzle_radius', motorRequest.nozzle_radius)",
-									"pm.environment.set('throat_radius', motorRequest.throat_radius)",
-									"pm.environment.set('interpolation_method', motorRequest.interpolation_method)",
-									"pm.environment.set('motor_coordinate_system_orientation', motorRequest.coordinate_system_orientation)",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Motor PUT request is made to the API\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Motor successfully updated\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid new_motor_id\", function () {",
-									"        pm.expect(apiRspn.new_motor_id).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						},
-						{
-							"listen": "prerequest",
-							"script": {
-								"exec": [
-									""
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "PUT",
-						"header": [],
-						"body": {
-							"mode": "raw",
-							"raw": "{\n  \"thrust_source\": \"Cesaroni_M1670\",\n  \"burn_time\": 3.9,\n  \"nozzle_radius\": 0.033,\n  \"dry_mass\": 1.815,\n  \"dry_inertia\": [\n    0.125,\n    0.125,\n    0.002\n  ],\n  \"center_of_dry_mass_position\": 0.317,\n  \"tanks\": [\n    {\n      \"discretize\": 100,\n      \"flux_time\": [\n        0,\n        8\n      ],\n      \"gas\": {\n        \"density\": 100,\n        \"name\": \"FluidName\"\n      },\n      \"gas_mass\": 0.1,\n      \"gas_mass_flow_rate_in\": 0.1,\n      \"gas_mass_flow_rate_out\": 0.1,\n      \"geometry\": [\n        [\n          [\n            0,\n            5\n          ],\n          1\n        ],\n        [\n          [\n            5,\n            10\n          ],\n          2\n        ]\n      ],\n      \"initial_gas_mass\": 0.1,\n      \"initial_liquid_mass\": 5,\n      \"liquid\": {\n        \"density\": 100,\n        \"name\": \"FluidName\"\n      },\n      \"liquid_height\": 0.5,\n      \"liquid_mass\": 5,\n      \"liquid_mass_flow_rate_in\": 0.1,\n      \"liquid_mass_flow_rate_out\": 0.1,\n      \"name\": \"Tank\",\n      \"position\": 1,\n      \"tank_kind\": \"MassFlow\",\n      \"ullage\": 0.1\n    }\n  ],\n  \"grain_number\": 5,\n  \"grain_density\": 1815,\n  \"grain_outer_radius\": 0.033,\n  \"grain_initial_inner_radius\": 0.015,\n  \"grain_initial_height\": 0.12,\n  \"grains_center_of_mass_position\": -0.85704,\n  \"grain_separation\": 0.005,\n  \"throat_radius\": 0.011,\n  \"interpolation_method\": \"linear\",\n  \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\"\n}",
-							"options": {
-								"raw": {
-									"language": "json"
-								}
-							}
-						},
-						"url": {
-							"raw": "{{endpoint}}/motors/{{motor_id}}/?motor_kind=Liquid",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"motors",
-								"{{motor_id}}",
-								""
-							],
-							"query": [
-								{
-									"key": "motor_kind",
-									"value": "Liquid"
-								}
-							]
-						},
-						"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-					},
-					"response": []
-				},
-				{
-					"name": "Delete Motor",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"//TEST",
-									"bdd = \"Given a valid Motor DELETE request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Motor successfully deleted\", \"message not matching\");",
-									"        pm.expect(apiRspn.deleted_motor_id).to.eql(pm.environment.get('motor_id'), \"motor_id not matching\");                ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "DELETE",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/motors/{{motor_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"motors",
-								"{{motor_id}}"
-							]
-						}
-					},
-					"response": []
-				}
-			]
-		},
-		{
-			"name": "Rocket",
-			"item": [
-				{
-					"name": "Create Rocket",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"var rocketRequest = JSON.parse(pm.request.body.raw);",
-									"",
-									"// save rocket parameters",
-									"pm.environment.set('rocket_id', apiRspn.rocket_id)",
-									"pm.environment.set('radius', rocketRequest.radius)",
-									"pm.environment.set('mass', rocketRequest.mass)",
-									"pm.environment.set('inertia', rocketRequest.inertia)",
-									"pm.environment.set('power_off_drag', rocketRequest.power_off_drag)",
-									"pm.environment.set('power_on_drag', rocketRequest.power_on_drag)",
-									"pm.environment.set('center_of_mass_without_motor', rocketRequest.center_of_mass_without_motor)",
-									"pm.environment.set('motor_position', rocketRequest.motor_position)",
-									"pm.environment.set('rail_buttons', rocketRequest.rail_buttons)",
-									"pm.environment.set('upper_button_position', rocketRequest.rail_buttons.upper_button_position)",
-									"pm.environment.set('lower_button_position', rocketRequest.rail_buttons.lower_button_position)",
-									"pm.environment.set('angular_position', rocketRequest.rail_buttons.angular_position)",
-									"pm.environment.set('rocket_coordinate_system_orientation', rocketRequest.coordinate_system_orientation)",
-									"",
-									"// rocket motor",
-									"pm.environment.set('burn_time', rocketRequest.motor.burn_time)",
-									"pm.environment.set('dry_mass', rocketRequest.motor.dry_mass)",
-									"pm.environment.set('dry_inertia', rocketRequest.motor.dry_inertia)",
-									"pm.environment.set('center_of_dry_mass_position', rocketRequest.motor.center_of_dry_mass_position)",
-									"pm.environment.set('grain_number', rocketRequest.motor.grain_number)",
-									"pm.environment.set('grain_density', rocketRequest.motor.grain_density)",
-									"pm.environment.set('grain_outer_radius', rocketRequest.motor.grain_outer_radius)",
-									"pm.environment.set('grain_initial_inner_radius', rocketRequest.motor.grain_initial_inner_radius)",
-									"pm.environment.set('grain_initial_height', rocketRequest.motor.grain_initial_height)",
-									"pm.environment.set('grains_center_of_mass_position', rocketRequest.motor.grains_center_of_mass_position)",
-									"pm.environment.set('grain_separation', rocketRequest.motor.grain_separation)",
-									"pm.environment.set('thrust_source', rocketRequest.motor.thrust_source)",
-									"pm.environment.set('nozzle_radius', rocketRequest.motor.nozzle_radius)",
-									"pm.environment.set('throat_radius', rocketRequest.motor.throat_radius)",
-									"pm.environment.set('interpolation_method', rocketRequest.motor.interpolation_method)",
-									"pm.environment.set('motor_coordinate_system_orientation', rocketRequest.motor.coordinate_system_orientation)",
-									"",
-									"// rocket nose",
-									"pm.environment.set('nose_length', rocketRequest.nose.length)",
-									"pm.environment.set('kind', rocketRequest.nose.kind)",
-									"pm.environment.set('nose_position', rocketRequest.nose.position)",
-									"pm.environment.set('base_radius', rocketRequest.nose.base_radius)",
-									"pm.environment.set('rocket_radius', rocketRequest.nose.rocket_radius)",
-									"",
-									"// rocket fins",
-									"pm.environment.set('n', rocketRequest.fins.n)",
-									"pm.environment.set('root_chord', rocketRequest.fins.root_chord)",
-									"pm.environment.set('tip_chord', rocketRequest.fins.tip_chord)",
-									"pm.environment.set('span', rocketRequest.fins.span)",
-									"pm.environment.set('fin_position', rocketRequest.fins.position)",
-									"pm.environment.set('cant_angle', rocketRequest.fins.cant_angle)",
-									"pm.environment.set('fin_radius', rocketRequest.fins.radius)",
-									"pm.environment.set('airfoil', rocketRequest.fins.airfoil)",
-									"",
-									"// rocket tail",
-									"pm.environment.set('top_radius', rocketRequest.tail.top_radius)",
-									"pm.environment.set('bottom_radius', rocketRequest.tail.bottom_radius)",
-									"pm.environment.set('tail_length', rocketRequest.tail.length)",
-									"pm.environment.set('tail_position', rocketRequest.tail.position)",
-									"pm.environment.set('tail_radius', rocketRequest.tail.radius)",
-									"",
-									"// rocket parachute",
-									"pm.environment.set('parachutes_names', rocketRequest.parachutes.name)",
-									"pm.environment.set('parachutes_cds', rocketRequest.parachutes.cd_s)",
-									"pm.environment.set('parachutes_sampling_rate', rocketRequest.parachutes.sampling_rate)",
-									"pm.environment.set('parachutes_lags', rocketRequest.parachutes.lag)",
-									"pm.environment.set('parachutes_noises', rocketRequest.parachutes.noise)",
-									"pm.environment.set('parachutes_triggers', rocketRequest.parachutes.triggers)",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Rocket POST request is made to the API\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Rocket successfully created\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid rocket_id\", function () {",
-									"        pm.expect(apiRspn.rocket_id).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						},
-						{
-							"listen": "prerequest",
-							"script": {
-								"exec": [
-									""
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "POST",
-						"header": [],
-						"body": {
-							"mode": "raw",
-							"raw": "{\n  \"rail_buttons\": {\n    \"angular_position\": 45,\n    \"lower_button_position\": 0.2,\n    \"upper_button_position\": -0.5\n  },\n  \"motor\": {\n    \"burn_time\": 3.9,\n    \"center_of_dry_mass_position\": 0.317,\n    \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n    \"dry_inertia\": [\n      0.125,\n      0.125,\n      0.002\n    ],\n    \"dry_mass\": 1.815,\n    \"grain_density\": 1815,\n    \"grain_initial_height\": 0.12,\n    \"grain_initial_inner_radius\": 0.015,\n    \"grain_number\": 5,\n    \"grain_outer_radius\": 0.033,\n    \"grain_separation\": 0.005,\n    \"grains_center_of_mass_position\": -0.85704,\n    \"interpolation_method\": \"linear\",\n    \"nozzle_radius\": 0.033,\n    \"tanks\": [\n      {\n        \"discretize\": 100,\n        \"flux_time\": [\n          0,\n          8\n        ],\n        \"gas\": {\n          \"density\": 100,\n          \"name\": \"FluidName\"\n        },\n        \"gas_mass\": 0.1,\n        \"gas_mass_flow_rate_in\": 0.1,\n        \"gas_mass_flow_rate_out\": 0.1,\n        \"geometry\": [\n          [\n            [\n              0,\n              5\n            ],\n            1\n          ],\n          [\n            [\n              5,\n              10\n            ],\n            2\n          ]\n        ],\n        \"initial_gas_mass\": 0.1,\n        \"initial_liquid_mass\": 5,\n        \"liquid\": {\n          \"density\": 100,\n          \"name\": \"FluidName\"\n        },\n        \"liquid_height\": 0.5,\n        \"liquid_mass\": 5,\n        \"liquid_mass_flow_rate_in\": 0.1,\n        \"liquid_mass_flow_rate_out\": 0.1,\n        \"name\": \"Tank\",\n        \"position\": 1,\n        \"tank_kind\": \"MassFlow\",\n        \"ullage\": 0.1\n      }\n    ],\n    \"throat_radius\": 0.011,\n    \"thrust_source\": \"Cesaroni_M1670\"\n  },\n  \"nose\": {\n    \"base_radius\": 0.0635,\n    \"kind\": \"vonKarman\",\n    \"length\": 0.55829,\n    \"position\": 1.278,\n    \"rocket_radius\": 0.0635\n  },\n  \"fins\": {\n    \"airfoil\": \"\",\n    \"cant_angle\": 0,\n    \"n\": 4,\n    \"position\": -1.04956,\n    \"radius\": 0.0635,\n    \"root_chord\": 0.12,\n    \"span\": 0.1,\n    \"tip_chord\": 0.04\n  },\n  \"tail\": {\n    \"bottom_radius\": 0.0435,\n    \"length\": 0.06,\n    \"position\": -1.194656,\n    \"radius\": 0.0635,\n    \"top_radius\": 0.0635\n  },\n  \"parachutes\": {\n    \"cd_s\": [\n      10,\n      1\n    ],\n    \"lag\": [\n      1.5,\n      1.5\n    ],\n    \"name\": [\n      \"Main\",\n      \"Drogue\"\n    ],\n    \"noise\": [\n      [\n        0,\n        8.3,\n        0.5\n      ],\n      [\n        0,\n        8.3,\n        0.5\n      ]\n    ],\n    \"sampling_rate\": [\n      105,\n      105\n    ],\n    \"triggers\": [\n      \"lambda p, h, y: y[5] < 0 and h < 800\",\n      \"lambda p, h, y: y[5] < 0\"\n    ]\n  },\n  \"inertia\": [\n    6.321,\n    6.321,\n    0.0346\n  ],\n  \"center_of_mass_without_motor\": 0,\n  \"radius\": 0.0632,\n  \"mass\": 16.235,\n  \"motor_position\": -1.255,\n  \"power_off_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"power_on_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"coordinate_system_orientation\": \"tail_to_nose\"\n}",
-							"options": {
-								"raw": {
-									"language": "json"
-								}
-							}
-						},
-						"url": {
-							"raw": "{{endpoint}}/rockets/?rocket_option=Calisto&motor_kind=Solid",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"rockets",
-								""
-							],
-							"query": [
-								{
-									"key": "rocket_option",
-									"value": "Calisto"
-								},
-								{
-									"key": "motor_kind",
-									"value": "Solid"
-								}
-							]
-						},
-						"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-					},
-					"response": []
-				},
-				{
-					"name": "Read Rocket",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Rocket GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });    ",
-									"    pm.test(bdd + \" then response must contain a valid rocket\", function () {        ",
-									"        pm.expect(apiRspn.radius).to.eql(pm.environment.get('radius'), \"rocket radius not matching\");",
-									"        pm.expect(apiRspn.mass).to.eql(pm.environment.get('mass'), \"rocket mass not matching\");",
-									"        pm.expect(apiRspn.inertia).to.eql(pm.environment.get('inertia'), \"rocket inertia not matching\");",
-									"        pm.expect(apiRspn.power_off_drag).to.eql(pm.environment.get('power_off_drag'), \"rocket power_off_drag not matching\");",
-									"        pm.expect(apiRspn.power_on_drag).to.eql(pm.environment.get('power_on_drag'), \"rocket power_on_drag not matching\");",
-									"        pm.expect(apiRspn.center_of_mass_without_motor).to.eql(pm.environment.get('center_of_mass_without_motor'), \"rocket center_of_mass_without_motor not matching\");",
-									"        pm.expect(apiRspn.coordinate_system_orientation).to.eql(pm.environment.get('rocket_coordinate_system_orientation'), \"rocket coordinate_system_orientation not matching\");",
-									"        pm.expect(apiRspn.motor_position).to.eql(pm.environment.get('motor_position'), \"rocket motor_position not matching\");",
-									"        pm.expect(apiRspn.rail_buttons).to.eql(pm.environment.get('rail_buttons'), \"rocket rail_buttons not matching\");",
-									"        pm.expect(apiRspn.rail_buttons.upper_button_position).to.eql(pm.environment.get('upper_button_position'), \"rocket rail_buttons upper_button_position not matching\");",
-									"        pm.expect(apiRspn.rail_buttons.lower_button_position).to.eql(pm.environment.get('lower_button_position'), \"rocket rail_buttons lower_button_position not matching\");",
-									"        pm.expect(apiRspn.rail_buttons.angular_position).to.eql(pm.environment.get('angular_position'), \"rocket rail_buttons angular_position not matching\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid flight rocket motor\", function () {",
-									"        pm.expect(apiRspn.motor.burn_time).to.eql(pm.environment.get('burn_time'), \"rocket motor burn_time not matching\");",
-									"        pm.expect(apiRspn.motor.dry_mass).to.eql(pm.environment.get('dry_mass'), \"rocket motor dry_mass not matching\");",
-									"        pm.expect(apiRspn.motor.dry_inertia).to.eql(pm.environment.get('dry_inertia'), \"rocket motor dry_inertia not matching\");",
-									"        pm.expect(apiRspn.motor.center_of_dry_mass_position).to.eql(pm.environment.get('center_of_dry_mass_position'), \"rocket motor center_of_dry_mass_position not matching\");",
-									"        pm.expect(apiRspn.motor.grain_number).to.eql(pm.environment.get('grain_number'), \"rocket motor grain_number not matching\");",
-									"        pm.expect(apiRspn.motor.grain_density).to.eql(pm.environment.get('grain_density'), \"rocket motor grain_density not matching\");",
-									"        pm.expect(apiRspn.motor.grain_outer_radius).to.eql(pm.environment.get('grain_outer_radius'), \"rocket motor grain_outer_radius not matching\");",
-									"        pm.expect(apiRspn.motor.grain_initial_inner_radius).to.eql(pm.environment.get('grain_initial_inner_radius'), \"rocket motor grain_initial_inner_radius not matching\");",
-									"        pm.expect(apiRspn.motor.grain_initial_height).to.eql(pm.environment.get('grain_initial_height'), \"rocket motor grain_initial_height not matching\");",
-									"        pm.expect(apiRspn.motor.grains_center_of_mass_position).to.eql(pm.environment.get('grains_center_of_mass_position'), \"rocket motor grains_center_of_mass_position not matching\");",
-									"        pm.expect(apiRspn.motor.thrust_source).to.eql(pm.environment.get('thrust_source'), \"rocket motor thrust_source not matching\");",
-									"        pm.expect(apiRspn.motor.grain_separation).to.eql(pm.environment.get('grain_separation'), \"rocket motor grain_separation not matching\");",
-									"        pm.expect(apiRspn.motor.nozzle_radius).to.eql(pm.environment.get('nozzle_radius'), \"rocket motor nozzle_radius not matching\");",
-									"        pm.expect(apiRspn.motor.throat_radius).to.eql(pm.environment.get('throat_radius'), \"rocket motor throat_radius not matching\");",
-									"        pm.expect(apiRspn.motor.interpolation_method).to.eql(pm.environment.get('interpolation_method'), \"rocket motor interpolation_method not matching\");",
-									"        pm.expect(apiRspn.motor.coordinate_system_orientation).to.eql(pm.environment.get('motor_coordinate_system_orientation'), \"motor coordinate_system_orientation not matching\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid flight rocket nose\", function () {",
-									"        pm.expect(apiRspn.nose.length).to.eql(pm.environment.get('nose_length'), \"rocket nose length not matching\");",
-									"        pm.expect(apiRspn.nose.kind).to.eql(pm.environment.get('kind'), \"rocket nose kind not matching\");",
-									"        pm.expect(apiRspn.nose.position).to.eql(pm.environment.get('nose_position'), \"rocket nose position not matching\");",
-									"        pm.expect(apiRspn.nose.base_radius).to.eql(pm.environment.get('base_radius'), \"rocket nose base_radius not matching\");",
-									"        pm.expect(apiRspn.nose.rocket_radius).to.eql(pm.environment.get('rocket_radius'), \"rocket nose rocket_radius not matching\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid flight rocket fins\", function () {",
-									"        pm.expect(apiRspn.fins.n).to.eql(pm.environment.get('n'), \"rocket fins 'n' not matching\");",
-									"        pm.expect(apiRspn.fins.root_chord).to.eql(pm.environment.get('root_chord'), \"rocket fins root_chord not matching\");",
-									"        pm.expect(apiRspn.fins.tip_chord).to.eql(pm.environment.get('tip_chord'), \"rocket fins tip_chord not matching\");",
-									"        pm.expect(apiRspn.fins.span).to.eql(pm.environment.get('span'), \"rocket fins span not matching\");",
-									"        pm.expect(apiRspn.fins.position).to.eql(pm.environment.get('fin_position'), \"rocket fins position not matching\");",
-									"        pm.expect(apiRspn.fins.cant_angle).to.eql(pm.environment.get('cant_angle'), \"rocket fins cant_angle not matching\");",
-									"        pm.expect(apiRspn.fins.radius).to.eql(pm.environment.get('fin_radius'), \"rocket fins radius not matching\");",
-									"        pm.expect(apiRspn.fins.airfoil).to.eql(pm.environment.get('airfoil'), \"rocket fins airfoil not matching\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid flight rocket tail\", function () {",
-									"        pm.expect(apiRspn.tail.top_radius).to.eql(pm.environment.get('top_radius'), \"rocket tail top_radius not matching\");        ",
-									"        pm.expect(apiRspn.tail.bottom_radius).to.eql(pm.environment.get('bottom_radius'), \"rocket tail bottom_radius not matching\");        ",
-									"        pm.expect(apiRspn.tail.length).to.eql(pm.environment.get('tail_length'), \"rocket tail length not matching\");        ",
-									"        pm.expect(apiRspn.tail.position).to.eql(pm.environment.get('tail_position'), \"rocket tail position not matching\");        ",
-									"        pm.expect(apiRspn.tail.radius).to.eql(pm.environment.get('tail_radius'), \"rocket tail radius not matching\");        ",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid flight rocket parachutes\", function () {",
-									"        pm.expect(apiRspn.parachutes.name).to.eql(pm.environment.get('parachutes_names'), \"rocket parachutes names not matching\");                ",
-									"        pm.expect(apiRspn.parachutes.cd_s).to.eql(pm.environment.get('parachutes_cds'), \"rocket parachutes cd_s not matching\");                ",
-									"        pm.expect(apiRspn.parachutes.sampling_rate).to.eql(pm.environment.get('parachutes_sampling_rate'), \"rocket parachutes sampling_rate not matching\");                ",
-									"        pm.expect(apiRspn.parachutes.lag).to.eql(pm.environment.get('parachutes_lags'), \"rocket parachutes lags not matching\");                ",
-									"        pm.expect(apiRspn.parachutes.noise).to.eql(pm.environment.get('parachutes_noises'), \"rocket parachutes noises not matching\");",
-									"        pm.expect(apiRspn.parachutes.triggers).to.eql(pm.environment.get('parachutes_triggers'), \"rocket parachutes triggers not matching\");",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/rockets/{{rocket_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"rockets",
-								"{{rocket_id}}"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Read rocketpy Rocket",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid rocketpy Rocket GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.jsonpickle_rocketpy_rocket).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/rockets/rocketpy/{{rocket_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"rockets",
-								"rocketpy",
-								"{{rocket_id}}"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Simulate Rocket",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"//TEST",
-									"bdd = \"Given a valid rocketpy Rocket simulate GET request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.rocket_data).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.inertia_details).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.inertia_details.rocket_mass_without_propellant).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.inertia_details.rocket_mass_with_propellant).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.inertia_details.rocket_inertia_with_motor_without_propellant).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_geometrical_parameters).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_geometrical_parameters.rocket_maximum_radius).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_geometrical_parameters.rocket_frontal_area).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_geometrical_parameters.rocket_codm_nozzle_exit_distance).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_geometrical_parameters.rocket_codm_center_of_propellant_mass).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_geometrical_parameters.rocket_codm_loaded_center_of_mass).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_aerodynamics_quantities).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_aerodynamics_quantities.aerodynamics_lift_coefficient_derivatives).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_aerodynamics_quantities.aerodynamics_center_of_pressure).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_aerodynamics_quantities.distance_cop_to_codm).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_aerodynamics_quantities.initial_static_margin).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.rocket_aerodynamics_quantities.final_static_margin).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.parachute_data).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.parachute_data.parachute_details).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.parachute_data.parachute_ejection_system_refresh_rate).to.exist;",
-									"        pm.expect(apiRspn.rocket_data.parachute_data.parachute_lag).to.exist;",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "GET",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/rockets/{{rocket_id}}/simulate",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"rockets",
-								"{{rocket_id}}",
-								"simulate"
-							]
-						}
-					},
-					"response": []
-				},
-				{
-					"name": "Update Rocket",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"var rocketRequest = JSON.parse(pm.request.body.raw);",
-									"",
-									"// save rocket parameters",
-									"pm.environment.set('rocket_id', apiRspn.new_rocket_id)",
-									"pm.environment.set('radius', rocketRequest.radius)",
-									"pm.environment.set('mass', rocketRequest.mass)",
-									"pm.environment.set('inertia', rocketRequest.inertia)",
-									"pm.environment.set('power_off_drag', rocketRequest.power_off_drag)",
-									"pm.environment.set('power_on_drag', rocketRequest.power_on_drag)",
-									"pm.environment.set('center_of_mass_without_motor', rocketRequest.center_of_mass_without_motor)",
-									"pm.environment.set('motor_position', rocketRequest.motor_position)",
-									"pm.environment.set('rail_buttons', rocketRequest.rail_buttons)",
-									"pm.environment.set('upper_button_position', rocketRequest.rail_buttons.upper_button_position)",
-									"pm.environment.set('lower_button_position', rocketRequest.rail_buttons.lower_button_position)",
-									"pm.environment.set('angular_position', rocketRequest.rail_buttons.angular_position)",
-									"pm.environment.set('rocket_coordinate_system_orientation', rocketRequest.coordinate_system_orientation)",
-									"",
-									"// rocket motor",
-									"pm.environment.set('burn_time', rocketRequest.motor.burn_time)",
-									"pm.environment.set('dry_mass', rocketRequest.motor.dry_mass)",
-									"pm.environment.set('dry_inertia', rocketRequest.motor.dry_inertia)",
-									"pm.environment.set('center_of_dry_mass_position', rocketRequest.motor.center_of_dry_mass_position)",
-									"pm.environment.set('grain_number', rocketRequest.motor.grain_number)",
-									"pm.environment.set('grain_density', rocketRequest.motor.grain_density)",
-									"pm.environment.set('grain_outer_radius', rocketRequest.motor.grain_outer_radius)",
-									"pm.environment.set('grain_initial_inner_radius', rocketRequest.motor.grain_initial_inner_radius)",
-									"pm.environment.set('grain_initial_height', rocketRequest.motor.grain_initial_height)",
-									"pm.environment.set('grains_center_of_mass_position', rocketRequest.motor.grains_center_of_mass_position)",
-									"pm.environment.set('grain_separation', rocketRequest.motor.grain_separation)",
-									"pm.environment.set('thrust_source', rocketRequest.motor.thrust_source)",
-									"pm.environment.set('nozzle_radius', rocketRequest.motor.nozzle_radius)",
-									"pm.environment.set('throat_radius', rocketRequest.motor.throat_radius)",
-									"pm.environment.set('interpolation_method', rocketRequest.motor.interpolation_method)",
-									"pm.environment.set('motor_coordinate_system_orientation', rocketRequest.motor.coordinate_system_orientation)",
-									"",
-									"// rocket nose",
-									"pm.environment.set('nose_length', rocketRequest.nose.length)",
-									"pm.environment.set('kind', rocketRequest.nose.kind)",
-									"pm.environment.set('nose_position', rocketRequest.nose.position)",
-									"pm.environment.set('base_radius', rocketRequest.nose.base_radius)",
-									"pm.environment.set('rocket_radius', rocketRequest.nose.rocket_radius)",
-									"",
-									"// rocket fins",
-									"pm.environment.set('n', rocketRequest.fins.n)",
-									"pm.environment.set('root_chord', rocketRequest.fins.root_chord)",
-									"pm.environment.set('tip_chord', rocketRequest.fins.tip_chord)",
-									"pm.environment.set('span', rocketRequest.fins.span)",
-									"pm.environment.set('fin_position', rocketRequest.fins.position)",
-									"pm.environment.set('cant_angle', rocketRequest.fins.cant_angle)",
-									"pm.environment.set('fin_radius', rocketRequest.fins.radius)",
-									"pm.environment.set('airfoil', rocketRequest.fins.airfoil)",
-									"",
-									"// rocket tail",
-									"pm.environment.set('top_radius', rocketRequest.tail.top_radius)",
-									"pm.environment.set('bottom_radius', rocketRequest.tail.bottom_radius)",
-									"pm.environment.set('tail_length', rocketRequest.tail.length)",
-									"pm.environment.set('tail_position', rocketRequest.tail.position)",
-									"pm.environment.set('tail_radius', rocketRequest.tail.radius)",
-									"",
-									"// rocket parachute",
-									"pm.environment.set('parachutes_names', rocketRequest.parachutes.name)",
-									"pm.environment.set('parachutes_cds', rocketRequest.parachutes.cd_s)",
-									"pm.environment.set('parachutes_sampling_rate', rocketRequest.parachutes.sampling_rate)",
-									"pm.environment.set('parachutes_lags', rocketRequest.parachutes.lag)",
-									"pm.environment.set('parachutes_noises', rocketRequest.parachutes.noise)",
-									"pm.environment.set('parachutes_triggers', rocketRequest.parachutes.triggers)",
-									"",
-									"//TEST",
-									"bdd = \"Given a valid Rocket PUT request is made to the API\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Rocket successfully updated\");",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid rocket_id\", function () {",
-									"        pm.expect(apiRspn.new_rocket_id).to.exist;        ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						},
-						{
-							"listen": "prerequest",
-							"script": {
-								"exec": [
-									""
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "PUT",
-						"header": [],
-						"body": {
-							"mode": "raw",
-							"raw": "{\n  \"rail_buttons\": {\n    \"angular_position\": 47,\n    \"lower_button_position\": 0.1,\n    \"upper_button_position\": -0.2\n  },\n  \"motor\": {\n    \"burn_time\": 5.9,\n    \"center_of_dry_mass_position\": 0.317,\n    \"coordinate_system_orientation\": \"nozzle_to_combustion_chamber\",\n    \"dry_inertia\": [\n      0.125,\n      0.125,\n      0.002\n    ],\n    \"dry_mass\": 1.815,\n    \"grain_density\": 1815,\n    \"grain_initial_height\": 0.12,\n    \"grain_initial_inner_radius\": 0.015,\n    \"grain_number\": 5,\n    \"grain_outer_radius\": 0.033,\n    \"grain_separation\": 0.005,\n    \"grains_center_of_mass_position\": -0.85704,\n    \"interpolation_method\": \"linear\",\n    \"nozzle_radius\": 0.033,\n    \"tanks\": [\n      {\n        \"discretize\": 100,\n        \"flux_time\": [\n          0,\n          8\n        ],\n        \"gas\": {\n          \"density\": 100,\n          \"name\": \"FluidName\"\n        },\n        \"gas_mass\": 0.1,\n        \"gas_mass_flow_rate_in\": 0.1,\n        \"gas_mass_flow_rate_out\": 0.1,\n        \"geometry\": [\n          [\n            [\n              0,\n              5\n            ],\n            1\n          ],\n          [\n            [\n              5,\n              10\n            ],\n            2\n          ]\n        ],\n        \"initial_gas_mass\": 0.1,\n        \"initial_liquid_mass\": 5,\n        \"liquid\": {\n          \"density\": 100,\n          \"name\": \"FluidName\"\n        },\n        \"liquid_height\": 0.5,\n        \"liquid_mass\": 5,\n        \"liquid_mass_flow_rate_in\": 0.1,\n        \"liquid_mass_flow_rate_out\": 0.1,\n        \"name\": \"Tank\",\n        \"position\": 1,\n        \"tank_kind\": \"MassFlow\",\n        \"ullage\": 0.1\n      }\n    ],\n    \"throat_radius\": 0.011,\n    \"thrust_source\": \"Cesaroni_M1670\"\n  },\n  \"nose\": {\n    \"base_radius\": 0.0635,\n    \"kind\": \"vonKarman\",\n    \"length\": 0.55829,\n    \"position\": 1.278,\n    \"rocket_radius\": 0.0635\n  },\n  \"fins\": {\n    \"airfoil\": \"\",\n    \"cant_angle\": 0,\n    \"n\": 4,\n    \"position\": -1.04956,\n    \"radius\": 0.0635,\n    \"root_chord\": 0.12,\n    \"span\": 0.1,\n    \"tip_chord\": 0.04\n  },\n  \"tail\": {\n    \"bottom_radius\": 0.0435,\n    \"length\": 0.06,\n    \"position\": -1.194656,\n    \"radius\": 0.0635,\n    \"top_radius\": 0.0635\n  },\n  \"parachutes\": {\n    \"cd_s\": [\n      10,\n      1\n    ],\n    \"lag\": [\n      1.5,\n      1.5\n    ],\n    \"name\": [\n      \"Main\",\n      \"Drogue\"\n    ],\n    \"noise\": [\n      [\n        0,\n        8.3,\n        0.5\n      ],\n      [\n        0,\n        8.3,\n        0.5\n      ]\n    ],\n    \"sampling_rate\": [\n      105,\n      105\n    ],\n    \"triggers\": [\n      \"lambda p, h, y: y[5] < 0 and h < 800\",\n      \"lambda p, h, y: y[5] < 0\"\n    ]\n  },\n  \"inertia\": [\n    6.321,\n    6.321,\n    0.0346\n  ],\n  \"center_of_mass_without_motor\": 0,\n  \"radius\": 0.0632,\n  \"mass\": 16.235,\n  \"motor_position\": -1.255,\n  \"power_off_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"power_on_drag\": [\n    [\n      0.01,\n      0.333865758\n    ],\n    [\n      0.02,\n      0.394981721\n    ],\n    [\n      0.03,\n      0.407756063\n    ]\n  ],\n  \"coordinate_system_orientation\": \"tail_to_nose\"\n}",
-							"options": {
-								"raw": {
-									"language": "json"
-								}
-							}
-						},
-						"url": {
-							"raw": "{{endpoint}}/rockets/{{rocket_id}}/?rocket_option=Calisto&motor_kind=Hybrid",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"rockets",
-								"{{rocket_id}}",
-								""
-							],
-							"query": [
-								{
-									"key": "rocket_option",
-									"value": "Calisto"
-								},
-								{
-									"key": "motor_kind",
-									"value": "Hybrid"
-								}
-							]
-						},
-						"description": "This returns a `token` that you can use to retrieve information later on.\n\nWe have included a test to confirm if a token is returned. We have also added test scripts to copy the token to the `token` collection variable. This makes it easy for us to reuse this token in other requests in the collection."
-					},
-					"response": []
-				},
-				{
-					"name": "Delete Rocket",
-					"event": [
-						{
-							"listen": "test",
-							"script": {
-								"exec": [
-									"//Fixes the issue of breaking the collection runner whenever an http 500 is received",
-									"if (responseCode.code == 500) {",
-									"    pm.test(\"Given a request is made then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    return",
-									"}",
-									"",
-									"var apiRspn = pm.response.json();",
-									"//TEST",
-									"bdd = \"Given a valid Rocket DELETE request is made\";",
-									"    pm.test(bdd + \" then response must return a 200 status code\", function () {",
-									"        pm.expect(responseCode.code).to.eql(200);",
-									"    });",
-									"    pm.test(bdd + \" then response must contain a valid message\", function () {",
-									"        pm.expect(apiRspn.message).to.eql(\"Rocket successfully deleted\", \"message not matching\");",
-									"        pm.expect(apiRspn.deleted_rocket_id).to.eql(pm.environment.get('rocket_id'), \"rocket_id not matching\");                ",
-									"    });"
-								],
-								"type": "text/javascript"
-							}
-						}
-					],
-					"request": {
-						"method": "DELETE",
-						"header": [],
-						"url": {
-							"raw": "{{endpoint}}/rockets/{{rocket_id}}",
-							"host": [
-								"{{endpoint}}"
-							],
-							"path": [
-								"rockets",
-								"{{rocket_id}}"
-							]
-						}
-					},
-					"response": []
-				}
-			]
-		}
-	],
-	"event": [
-		{
-			"listen": "prerequest",
-			"script": {
-				"type": "text/javascript",
-				"exec": [
-					""
-				]
-			}
-		},
-		{
-			"listen": "test",
-			"script": {
-				"type": "text/javascript",
-				"exec": [
-					""
-				]
-			}
-		}
-	],
-	"variable": [
-		{
-			"key": "env_id",
-			"value": ""
-		},
-		{
-			"key": "latitude",
-			"value": ""
-		},
-		{
-			"key": "longitude",
-			"value": ""
-		},
-		{
-			"key": "elevation",
-			"value": ""
-		},
-		{
-			"key": "standard_atmosphere",
-			"value": ""
-		},
-		{
-			"key": "atmospheric_model_type",
-			"value": ""
-		},
-		{
-			"key": "atmospheric_model_file",
-			"value": ""
-		},
-		{
-			"key": "date",
-			"value": ""
-		},
-		{
-			"key": "rail_length",
-			"value": ""
-		},
-		{
-			"key": "inclination",
-			"value": ""
-		},
-		{
-			"key": "heading",
-			"value": ""
-		},
-		{
-			"key": "flight_id",
-			"value": ""
-		},
-		{
-			"key": "radius",
-			"value": ""
-		},
-		{
-			"key": "mass",
-			"value": ""
-		},
-		{
-			"key": "inertia",
-			"value": ""
-		},
-		{
-			"key": "power_off_drag",
-			"value": ""
-		},
-		{
-			"key": "power_on_drag",
-			"value": ""
-		},
-		{
-			"key": "center_of_mass_without_motor",
-			"value": ""
-		},
-		{
-			"key": "motor_position",
-			"value": ""
-		},
-		{
-			"key": "rail_buttons",
-			"value": ""
-		},
-		{
-			"key": "upper_button_position",
-			"value": ""
-		},
-		{
-			"key": "lower_button_position",
-			"value": ""
-		},
-		{
-			"key": "angular_position",
-			"value": ""
-		},
-		{
-			"key": "burn_time",
-			"value": ""
-		},
-		{
-			"key": "dry_mass",
-			"value": ""
-		},
-		{
-			"key": "dry_inertia",
-			"value": ""
-		},
-		{
-			"key": "center_of_dry_mass_position",
-			"value": ""
-		},
-		{
-			"key": "grain_number",
-			"value": ""
-		},
-		{
-			"key": "grain_density",
-			"value": ""
-		},
-		{
-			"key": "grain_outer_radius",
-			"value": ""
-		},
-		{
-			"key": "grain_initial_inner_radius",
-			"value": ""
-		},
-		{
-			"key": "grain_initial_height",
-			"value": ""
-		},
-		{
-			"key": "grains_center_of_mass_position",
-			"value": ""
-		},
-		{
-			"key": "grain_separation",
-			"value": ""
-		},
-		{
-			"key": "thrust_source",
-			"value": ""
-		},
-		{
-			"key": "nozzle_radius",
-			"value": ""
-		},
-		{
-			"key": "throat_radius",
-			"value": ""
-		},
-		{
-			"key": "interpolation_method",
-			"value": ""
-		},
-		{
-			"key": "coordinate_system_orientation",
-			"value": ""
-		},
-		{
-			"key": "length",
-			"value": ""
-		},
-		{
-			"key": "kind",
-			"value": ""
-		},
-		{
-			"key": "position",
-			"value": ""
-		},
-		{
-			"key": "base_radius",
-			"value": ""
-		},
-		{
-			"key": "rocket_radius",
-			"value": ""
-		},
-		{
-			"key": "n",
-			"value": ""
-		},
-		{
-			"key": "root_chord",
-			"value": ""
-		},
-		{
-			"key": "tip_chord",
-			"value": ""
-		},
-		{
-			"key": "span",
-			"value": ""
-		},
-		{
-			"key": "cant_angle",
-			"value": ""
-		},
-		{
-			"key": "airfoil",
-			"value": ""
-		},
-		{
-			"key": "top_radius",
-			"value": ""
-		},
-		{
-			"key": "bottom_radius",
-			"value": ""
-		},
-		{
-			"key": "parachutes_names",
-			"value": ""
-		},
-		{
-			"key": "parachutes_cds",
-			"value": ""
-		},
-		{
-			"key": "parachutes_sampling_rate",
-			"value": ""
-		},
-		{
-			"key": "parachutes_lags",
-			"value": ""
-		},
-		{
-			"key": "parachutes_noises",
-			"value": ""
-		},
-		{
-			"key": "parachutes_triggers",
-			"value": ""
-		},
-		{
-			"key": "nose_length",
-			"value": ""
-		},
-		{
-			"key": "nose_position",
-			"value": ""
-		},
-		{
-			"key": "fin_position",
-			"value": ""
-		},
-		{
-			"key": "fin_radius",
-			"value": ""
-		},
-		{
-			"key": "tail_length",
-			"value": ""
-		},
-		{
-			"key": "tail_position",
-			"value": ""
-		},
-		{
-			"key": "tail_radius",
-			"value": ""
-		},
-		{
-			"key": "rocket_coordinate_system_orientation",
-			"value": ""
-		},
-		{
-			"key": "motor_coordinate_system_orientation",
-			"value": ""
-		},
-		{
-			"key": "motor_id",
-			"value": ""
-		},
-		{
-			"key": "rocket_id",
-			"value": ""
-		}
-	]
-}
\ No newline at end of file