From 49790c6b6b3fc5af7faeaadd5c1f918552ce4995 Mon Sep 17 00:00:00 2001 From: SkyPhoenix999 <54157874+SkyPhoenix999@users.noreply.github.com> Date: Sun, 11 Aug 2024 13:32:12 -0400 Subject: [PATCH] New Raptor and RVac MECs (#2991) * New Raptor and RVac MEC - Updated Specs for Raptor - Split off RVac into separate Config - Changed to support Raptor 1, Raptor 2, and Raptor 3. * Changed Spaces to Dashes Changed Spaces to Dashes because RP-1 hates spaces * Borked Link * Also a Borked Link * Update CryoEngines Raptor Configs --- .../Engine_Configs/Raptor_Config.cfg | 201 ++++++------ .../Engine_Configs/Raptor_Vac_Config.cfg | 296 ++++++++++++++++++ .../CryoEngines/RO_CryoEngines_Engines.cfg | 44 +-- 3 files changed, 405 insertions(+), 136 deletions(-) create mode 100644 GameData/RealismOverhaul/Engine_Configs/Raptor_Vac_Config.cfg diff --git a/GameData/RealismOverhaul/Engine_Configs/Raptor_Config.cfg b/GameData/RealismOverhaul/Engine_Configs/Raptor_Config.cfg index bc2ce60867..b64260b364 100644 --- a/GameData/RealismOverhaul/Engine_Configs/Raptor_Config.cfg +++ b/GameData/RealismOverhaul/Engine_Configs/Raptor_Config.cfg @@ -4,85 +4,87 @@ // Manufacturer: SpaceX // // ================================================================================= -// Raptor -// Superheavy - Starship +// Raptor-1 +// Starship (Starhopper - SN15) // -// Dry Mass: ~ 107 TWR Ratio +// Dry Mass: 2,080 kg (3,630kg Vehicle Side) // Thrust (SL): 1650 kN -// Thrust (Vac): 1800 kN -// ISP: 325 SL / 350 Vac +// Thrust (Vac): 1814.23 kN (185tf) +// ISP: 330 SL / 350 Vac // Burn Time: ??? // Chamber Pressure: 27.5 MPa -// Propellant: LOX / CH4 +// Propellant: Subcooled LOX / Subcooled CH4 // Prop Ratio: 3.55 // Throttle: 40% - 100% // Nozzle Ratio: 40 -// Ignitions: Almost Unlimited due to Torch-lit System +// Ignitions: Unlimited (Torch Igniter) // ================================================================================= -// Raptor Non-Throttleable -// Superheavy +// Raptor-2 +// Starship/Superheavy (Starship Block 1) // -// Dry Mass: ~ 107 TWR Ratio -// Thrust (SL): 3000 kN -// Thrust (Vac): 3200 kN -// ISP: 325 SL / 350 Vac +// Dry Mass: 1,630 kg (2,875kg Vehicle Side) +// Thrust (SL): ??? kN +// Thrust (Vac): 2255.53 kN (230tf) +// ISP: 328 SL / 347 Vac // Burn Time: ??? -// Chamber Pressure: 27.5 MPa -// Propellant: LOX / CH4 +// Chamber Pressure: 30 MPa +// Propellant: Subcooled LOX / Subcooled CH4 // Prop Ratio: 3.55 -// Throttle: 100% +// Throttle: 40% - 100% // Nozzle Ratio: 40 -// Ignitions: Almost Unlimited due to Torch-lit System +// Ignitions: Unlimited // ================================================================================= -// Raptor Vac -// Starship +// Raptor-3 +// Starship/Superheavy (Starship Block 2) // -// Dry Mass: ~ 107 TWR Ratio -// Thrust (SL): ??? -// Thrust (Vac): 2240.0 kN ~ Guess -// ISP: 240 SL / 380 Vac ~ Guess +// Dry Mass: 1,525 kg (1,720kg Vehicle Side) +// Thrust (SL): ??? kN +// Thrust (Vac): 2745.862 kN (280tf) +// ISP: 330 SL / 350 Vac // Burn Time: ??? -// Chamber Pressure: 33 MPa [2] -// Propellant: LOX / CH4 +// Chamber Pressure: 33+ MPa +// Propellant: Subcooled LOX / Subcooled CH4 // Prop Ratio: 3.55 // Throttle: 40% - 100% -// Nozzle Ratio: 107 [4] -// Ignitions: Almost Unlimited due to Torch-lit System +// Nozzle Ratio: 40 +// Ignitions: Unlimited // ================================================================================= // Sources: // [1] Propellant Ratio https://twitter.com/elonmusk/status/1258580078218412033 // [2] Chamber Pressure https://twitter.com/elonmusk/status/1295495834998513664 -// [3] Raptor Thrust/ Throttle Limit https://twitter.com/elonmusk/status/1295553672454311941 -// [4] Raptor Vac Expansion Ratio https://twitter.com/elonmusk/status/1309385646033842176 +// [3] Raptor-Thrust/ Throttle Limit https://twitter.com/elonmusk/status/1295553672454311941 +// [4] Raptor-Vac Expansion Ratio https://twitter.com/elonmusk/status/1309385646033842176 // [5] Torch-Lit System https://www.teslarati.com/spacex-scrubs-final-starhopper-flight-test-elon-musk/ // [6] Raptor https://youtu.be/-8p2JDTd13k?t=1213 -// [7] Raptor/Non-Throttleable https://youtu.be/-8p2JDTd13k?t=1085 -// [8] ~ Booster Outer Ring Raptors No Gimbal https://spaceflight101.com/spx/spacex-raptor/ +// [7] Raptor-1 and Raptor-2 Specs https://x.com/SpaceX/status/1819795288116330594 +// [8] Raptor-3 Specs https://x.com/SpaceX/status/1819772716339339664 // Used by: -// * ROEngines - -// Notes: +// ROEngines +// CryoEngines +// StarshipExpansionProject -// * WIP Config Subject to New Info/Specs // ================================================== @PART[*]:HAS[#engineType[Raptor]]:FOR[RealismOverhaulEngines] { %title = #roRaptorTitle //Raptor %manufacturer = #roMfrSpaceX - %description = #roRaptorDesc //The Raptor is a methalox full-flow staged combustion engine designed for both Starship & the Super Heavy Launch Vehicle. The Super Heavy first stage uses 31 sea-level optimized engines, and Starship uses 3 sea-level engines and 3 vacuum engines. + %description = #roRaptorDesc //The Raptor-is a methalox full-flow staged combustion engine designed for both Starship & the Super Heavy Launch Vehicle. The Super Heavy first stage uses 33 sea-level optimized engines, and Starship uses 3 sea-level engines and 3 vacuum engines. - @tags ^= :$: USA spacex raptor liquid pump booster upper lqdmethane lqdoxygen + @tags ^= :$: USA spacex Raptor-liquid pump booster upper cooledlqdmethane lqdmethane cooledlqdoxygen lqdoxygen - %specLevel = prototype //Still under development, no solid numbers at the moment? + %specLevel = operational - @MODULE[ModuleEngines*] + @MODULE[ModuleGimbal] { - %EngineType = LiquidFuel + %gimbalRangeXP = 15 + %gimbalRangeXN = 15 + %useGimbalResponseSpeed = true + %gimbalResponseSpeed = 16 } !MODULE[ModuleEngineConfigs],*{} @@ -100,38 +102,40 @@ { name = ModuleEngineConfigs type = ModuleEngines - configuration = Raptor + configuration = Raptor-1 modded = false - origMass = 1.5 + origMass = 2.08 CONFIG { - name = Raptor //[6] - specLevel = prototype - maxThrust = 1650 - minThrust = 660 // 40% throttle [3] + name = Raptor-1 + specLevel = operational + maxThrust = 1814.23 + minThrust = 725.692 // 40% throttle [3] heatProduction = 100 + ratedBurnTime = 1800 + throttleResponseRate = 0.625 + massMult = 1.0 // 2,080kg [7] PROPELLANT // Ratio = 3.55 [1] { - name = LqdMethane + name = CooledLqdMethane ratio = 0.4303 DrawGauge = true } PROPELLANT { - name = LqdOxygen + name = CooledLqdOxygen ratio = 0.5697 } atmosphereCurve { key = 0 350 - key = 1 325 + key = 1 330 } ullage = True pressureFed = False ignitions = 0 - gimbalRange = 8 // ~ ? IGNITOR_RESOURCE { @@ -140,152 +144,153 @@ } IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] { - name = LqdMethane + name = CooledLqdMethane amount = 0.43 // ~ Guess } IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] { - name = LqdOxygen + name = CooledLqdOxygen amount = 0.57 // ~ Guess } - - massMult = 1.0 - TESTFLIGHT:NEEDS[TestLite|TestFlight] { ratedBurnTime = 1800 // ~ Guess to Allow it to Burn For 30 Minutes - // assume roughly exponential relationship between chamber pressure and lifespan thrustModifier { key = 0.00 0.05 0 0 key = 1.00 1.00 3 3 } - - ignitionReliabilityStart = 0.98 // ~ Slight Chance of the Torch-lit system failing - ignitionReliabilityEnd = 0.995 // ~ Slight Chance of the Torch-lit system failing - cycleReliabilityStart = 0.99975 + ignitionReliabilityStart = 0.95 // ~ Slight Chance of the Torch-lit system failing + ignitionReliabilityEnd = 0.98 // ~ Slight Chance of the Torch-lit system failing + cycleReliabilityStart = 0.9 cycleReliabilityEnd = 0.99995 } } CONFIG { - name = Raptor Non-Throttleable // [7] - specLevel = prototype - maxThrust = 3000 - minThrust = 3000 + name = Raptor-2 + specLevel = operational + description = Second Generation Raptor-Engine, heavily simplified, lighter, and with uprated thrust. + maxThrust = 2255.5295 + minThrust = 902.2118 // 40% throttle [3] heatProduction = 100 + ratedBurnTime = 1800 + throttleResponseRate = 0.625 + massMult = 0.7788 // 1,630kg [7] PROPELLANT // Ratio = 3.55 [1] { - name = LqdMethane + name = CooledLqdMethane ratio = 0.4303 DrawGauge = true } PROPELLANT { - name = LqdOxygen + name = CooledLqdOxygen ratio = 0.5697 } atmosphereCurve { - key = 0 350 - key = 1 325 + key = 0 347 + key = 1 328 } ullage = True pressureFed = False ignitions = 0 - gimbalRange = 0 // [8] IGNITOR_RESOURCE { name = ElectricCharge amount = 1.0 } - IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + IGNITOR_RESOURCE { - name = LqdMethane - amount = 0.43 // ~ Guess + name = CooledLqdMethane + amount = 0.4303 // ~ Guess } - IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + IGNITOR_RESOURCE { - name = LqdOxygen - amount = 0.57 // ~ Guess + name = CooledLqdOxygen + amount = 0.5697 // ~ Guess } - - massMult = 1.15 // ~ Guess to Make it a Little More Heavier then the Less Powerful Throttleable Raptor - TESTFLIGHT:NEEDS[TestLite|TestFlight] { ratedBurnTime = 1800 // ~ Guess to Allow it to Burn For 30 Minutes + // assume roughly exponential relationship between chamber pressure and lifespan + thrustModifier + { + key = 0.00 0.05 0 0 + key = 1.00 1.00 3 3 + } ignitionReliabilityStart = 0.98 // ~ Slight Chance of the Torch-lit system failing ignitionReliabilityEnd = 0.995 // ~ Slight Chance of the Torch-lit system failing cycleReliabilityStart = 0.99975 cycleReliabilityEnd = 0.99995 + techTransfer = Raptor-1,Raptor-1 Vacuum:50 } } CONFIG { - name = Raptor Vacuum + name = Raptor-3 specLevel = prototype - maxThrust = 2240.0 // ~ Guess - minThrust = 896.0 // 40% throttle [3] + description = Third Generation Raptor-Engine with even greater simplification and even greater thrust, slightly heavier to include built in heatshielding. + maxThrust = 2745.862 + minThrust = 1098.3448 // 40% throttle [3] heatProduction = 100 + ratedBurnTime = 3600 + throttleResponseRate = 0.625 + massMult = 0.733173 // 1,525kg [8] PROPELLANT // Ratio = 3.55 [1] { - name = LqdMethane - ratio = 0.43 + name = CooledLqdMethane + ratio = 0.4303 DrawGauge = true } PROPELLANT { - name = LqdOxygen - ratio = 0.57 + name = CooledLqdOxygen + ratio = 0.5697 } atmosphereCurve { - key = 0 380 - key = 1 240 // ~ Guess + key = 0 350 + key = 1 330 } ullage = True pressureFed = False ignitions = 0 - gimbalRange = 6 // ~ Guess IGNITOR_RESOURCE { name = ElectricCharge amount = 1.0 } - IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + IGNITOR_RESOURCE { - name = LqdMethane + name = CooledLqdMethane amount = 0.4303 // ~ Guess } - IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + IGNITOR_RESOURCE { - name = LqdOxygen + name = CooledLqdOxygen amount = 0.5697 // ~ Guess } - - massMult = 1.25 // ~ Guess - TESTFLIGHT:NEEDS[TestLite|TestFlight] { - ratedBurnTime = 3600 // ~ Guess to Allow it to Burn For 1 Hour - + ratedBurnTime = 3600 // ~ Guess to Allow it to Burn For 1 Hour (For HLS?) // assume roughly exponential relationship between chamber pressure and lifespan thrustModifier { key = 0.00 0.05 0 0 key = 1.00 1.00 3 3 } - ignitionReliabilityStart = 0.98 // ~ Slight Chance of the Torch-lit system failing ignitionReliabilityEnd = 0.995 // ~ Slight Chance of the Torch-lit system failing cycleReliabilityStart = 0.99975 cycleReliabilityEnd = 0.99995 + techTransfer = Raptor-1,Raptor-2,Raptor-1 Vacuum,Raptor-2 Vacuum:50 } } } diff --git a/GameData/RealismOverhaul/Engine_Configs/Raptor_Vac_Config.cfg b/GameData/RealismOverhaul/Engine_Configs/Raptor_Vac_Config.cfg new file mode 100644 index 0000000000..a41360098f --- /dev/null +++ b/GameData/RealismOverhaul/Engine_Configs/Raptor_Vac_Config.cfg @@ -0,0 +1,296 @@ +// ================================================== +// Raptor-Vacuum (RVac) +// +// Manufacturer: SpaceX +// +// ================================================================================= +// Raptor-1-Vacuum +// Starship (SN20) +// +// Dry Mass: ??? kg +// Thrust (SL): ??? kN +// Thrust (Vac): 1961.33 kN (200tf) +// ISP: ??? SL / 380 Vac +// Burn Time: ??? +// Chamber Pressure: 27.5 MPa +// Propellant: Subcooled LOX / Subcooled CH4 +// Prop Ratio: 3.55 +// Throttle: 40% - 100% +// Nozzle Ratio: 40 +// Ignitions: Unlimited (Torch Igniter) +// ================================================================================= +// Raptor-2-Vacuum +// Starship (Starship Block 1) +// +// Dry Mass: ??? kg +// Thrust (SL): ??? kN +// Thrust (Vac): 2530.1157 kN (258tf) +// ISP: ??? SL / 378 Vac +// Burn Time: ??? +// Chamber Pressure: 30 MPa +// Propellant: Subcooled LOX / Subcooled CH4 +// Prop Ratio: 3.55 +// Throttle: 40% - 100% +// Nozzle Ratio: 40 +// Ignitions: Unlimited +// ================================================================================= +// Raptor-3-Vacuum +// Starship (Starship Block 2) +// +// Dry Mass: ??? kg +// Thrust (SL): ??? kN +// Thrust (Vac): 3000.8349 kN (306tf) +// ISP: ??? SL / 380 Vac +// Burn Time: ??? +// Chamber Pressure: 33+ MPa +// Propellant: Subcooled LOX / Subcooled CH4 +// Prop Ratio: 3.55 +// Throttle: 40% - 100% +// Nozzle Ratio: 40 +// Ignitions: Unlimited +// ================================================================================= + +// Sources: + +// [1] Propellant Ratio https://twitter.com/elonmusk/status/1258580078218412033 +// [2] Chamber Pressure https://twitter.com/elonmusk/status/1295495834998513664 +// [3] Raptor-Thrust/ Throttle Limit https://twitter.com/elonmusk/status/1295553672454311941 +// [4] Raptor-Vac Expansion Ratio https://twitter.com/elonmusk/status/1309385646033842176 +// [5] Torch-Lit System https://www.teslarati.com/spacex-scrubs-final-starhopper-flight-test-elon-musk/ +// [6] Raptor https://youtu.be/-8p2JDTd13k?t=1213 +// [7] Raptor-1 and Raptor-2 Specs https://x.com/SpaceX/status/1819795288116330594 +// [8] Raptor-3 Specs https://x.com/SpaceX/status/1819772716339339664 + +// Used by: + +// ROEngines +// CryoEngines +// StarshipExpansionProject + +// ================================================== + +@PART[*]:HAS[#engineType[RVac]]:FOR[RealismOverhaulEngines] +{ + %title = Raptor-Vacuum + %manufacturer = #roMfrSpaceX + %description = #roRaptorDesc //The Raptor-is a methalox full-flow staged combustion engine designed for both Starship & the Super Heavy Launch Vehicle. The Super Heavy first stage uses 33 sea-level optimized engines, and Starship uses 3 sea-level engines and 3-Vacuum engines. + + @tags ^= :$: USA spacex Raptor-liquid pump booster upper cooledlqdmethane lqdmethane cooledlqdoxygen lqdoxygen + + %specLevel = operational + + @MODULE[ModuleGimbal] + { + %gimbalRangeXP = 15 + %gimbalRangeXN = 15 + %useGimbalResponseSpeed = true + %gimbalResponseSpeed = 16 + } + + !MODULE[ModuleEngineConfigs],*{} + !MODULE[ModuleAlternator],*{} + !RESOURCE,*{} + + @MODULE[ModuleGimbal] + { + %gimbalRange = 8 + %useGimbalResponseSpeed = true + %gimbalResponseSpeed = 16 + } + + MODULE + { + name = ModuleEngineConfigs + type = ModuleEngines + configuration = Raptor-1-Vacuum + modded = false + origMass = 2.08 + CONFIG + { + name = Raptor-1-Vacuum + specLevel = operational + maxThrust = 1961.33 + minThrust = 784.532 // 40% throttle [3] + heatProduction = 100 + ratedBurnTime = 3600 + throttleResponseRate = 0.625 + massMult = 1.4 // ~ Guess (Assume 40% heavier than SL) + PROPELLANT // Ratio = 3.55 [1] + { + name = CooledLqdMethane + ratio = 0.43 + DrawGauge = true + } + PROPELLANT + { + name = CooledLqdOxygen + ratio = 0.57 + } + atmosphereCurve + { + key = 0 380 + key = 1 240 // ~ Guess + } + + ullage = True + pressureFed = False + ignitions = 0 + + IGNITOR_RESOURCE + { + name = ElectricCharge + amount = 1.0 + } + IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + { + name = CooledLqdMethane + amount = 0.4303 // ~ Guess + } + IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + { + name = CooledLqdOxygen + amount = 0.5697 // ~ Guess + } + TESTFLIGHT:NEEDS[TestLite|TestFlight] + { + ratedBurnTime = 3600 // ~ Guess to Allow it to Burn For 1 Hour + // assume roughly exponential relationship between chamber pressure and lifespan + thrustModifier + { + key = 0.00 0.05 0 0 + key = 1.00 1.00 3 3 + } + ignitionReliabilityStart = 0.98 // ~ Slight Chance of the Torch-lit system failing + ignitionReliabilityEnd = 0.995 // ~ Slight Chance of the Torch-lit system failing + cycleReliabilityStart = 0.99975 + cycleReliabilityEnd = 0.99995 + } + } + CONFIG + { + name = Raptor-2-Vacuum + specLevel = operational + description = Second Generation Raptor-Engine, heavily simplified, lighter, and with uprated thrust. + maxThrust = 2530.1157 + minThrust = 1012.04628 // 40% throttle [3] + heatProduction = 100 + ratedBurnTime = 3600 + throttleResponseRate = 0.625 + massMult = 1.09032 // ~ Guess (Assume 40% heavier than SL) + PROPELLANT // Ratio = 3.55 [1] + { + name = CooledLqdMethane + ratio = 0.43 + DrawGauge = true + } + PROPELLANT + { + name = CooledLqdOxygen + ratio = 0.57 + } + atmosphereCurve + { + key = 0 378 + key = 1 240 // ~ Guess + } + + ullage = True + pressureFed = False + ignitions = 0 + + IGNITOR_RESOURCE + { + name = ElectricCharge + amount = 1.0 + } + IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + { + name = CooledLqdMethane + amount = 0.4303 // ~ Guess + } + IGNITOR_RESOURCE // Torch-Lit System uses the same propellant has the engines [5] + { + name = CooledLqdOxygen + amount = 0.5697 // ~ Guess + } + TESTFLIGHT:NEEDS[TestLite|TestFlight] + { + ratedBurnTime = 3600 // ~ Guess to Allow it to Burn For 1 Hour + // assume roughly exponential relationship between chamber pressure and lifespan + thrustModifier + { + key = 0.00 0.05 0 0 + key = 1.00 1.00 3 3 + } + ignitionReliabilityStart = 0.98 // ~ Slight Chance of the Torch-lit system failing + ignitionReliabilityEnd = 0.995 // ~ Slight Chance of the Torch-lit system failing + cycleReliabilityStart = 0.99975 + cycleReliabilityEnd = 0.99995 + techTransfer = Raptor-1,Raptor-1-Vacuum:50 + } + } + CONFIG + { + name = Raptor-3-Vacuum + specLevel = prototype + description = Third Generation Raptor-Engine with even greater simplification and even greater thrust, slightly heavier to include built in heatshielding. + maxThrust = 3000.8349 + minThrust = 1200.33396 // 40% throttle [3] + heatProduction = 100 + ratedBurnTime = 3600 + throttleResponseRate = 0.625 + massMult = 1.0264422 // ~ Guess (Assume 40% heavier than SL) + PROPELLANT // Ratio = 3.55 [1] + { + name = CooledLqdMethane + ratio = 0.4303 + DrawGauge = true + } + PROPELLANT + { + name = CooledLqdOxygen + ratio = 0.5697 + } + atmosphereCurve + { + key = 0 380 + key = 1 240 + } + + ullage = True + pressureFed = False + ignitions = 0 + + IGNITOR_RESOURCE + { + name = ElectricCharge + amount = 1.0 + } + IGNITOR_RESOURCE + { + name = CooledLqdMethane + amount = 0.4303 // ~ Guess + } + IGNITOR_RESOURCE + { + name = CooledLqdOxygen + amount = 0.5697 // ~ Guess + } + TESTFLIGHT:NEEDS[TestLite|TestFlight] + { + ratedBurnTime = 3600 // ~ Guess to Allow it to Burn For 1 Hour + // assume roughly exponential relationship between chamber pressure and lifespan + thrustModifier + { + key = 0.00 0.05 0 0 + key = 1.00 1.00 3 3 + } + ignitionReliabilityStart = 0.98 // ~ Slight Chance of the Torch-lit system failing + ignitionReliabilityEnd = 0.995 // ~ Slight Chance of the Torch-lit system failing + cycleReliabilityStart = 0.99975 + cycleReliabilityEnd = 0.99995 + techTransfer = Raptor-1,Raptor-2,Raptor-1-Vacuum,Raptor-2-Vacuum:50 + } + } + } +} diff --git a/GameData/RealismOverhaul/RO_SuggestedMods/CryoEngines/RO_CryoEngines_Engines.cfg b/GameData/RealismOverhaul/RO_SuggestedMods/CryoEngines/RO_CryoEngines_Engines.cfg index e12830d428..a387ade9b9 100644 --- a/GameData/RealismOverhaul/RO_SuggestedMods/CryoEngines/RO_CryoEngines_Engines.cfg +++ b/GameData/RealismOverhaul/RO_SuggestedMods/CryoEngines/RO_CryoEngines_Engines.cfg @@ -36,13 +36,13 @@ // Remove all RL10 configs except B-2 and C-2 -@PART[cryoengine-hecate-1]:AFTER[RealismOverhaulEngines] +@PART[cryoengine-hecate-1]:AFTER[RealismOverhaulEngines] { %title = RL10B-2/C-2 %description = 1990s low-medium TWR, vacuum use. Developed for the Delta Cryogenic Second Stage (DCSS), which was first used on the Delta III then modified for the Delta IV. Its extending nozzle increases specific impulse compared to the RL10A, at the cost of greater dry mass. Boeing purchased a large number of these engines for the Delta IV, but the launcher's low flight rate led to ULA converting many of them to RL10C-1 engines for use on the Atlas V's Centaur upper stage. Min. stage diameter 2.0m - @MODULE[ModuleEngineConfigs] - { + @MODULE[ModuleEngineConfigs] + { @configuration = RL10B-2 !CONFIG[*]:HAS[#name[RL10A*]] {} !CONFIG[*]:HAS[#name[RL10C-1*]] {} @@ -83,7 +83,7 @@ %RSSROConfig = True @rescaleFactor = 1.3333 // Actually 1.461, but this way we keep the shroud at 5 meters for use on Delta IV's CBC %engineType = RS68 - + @MODULE[ModuleEngines*] { // Values from Rocket Propulsion Elements by Sutton @@ -173,16 +173,6 @@ %engineType = Raptor } -@PART[cryoengine-deinonychus-1]:FOR[RealismOverhaulEnginesPost] -{ - @title = Raptor (Surface Variant) - - @MODULE[ModuleEngineConfigs] - { - !CONFIG[Raptor?Vacuum] {} - } -} - //============= // Raptor Vac //============= @@ -191,19 +181,7 @@ { %RSSROConfig = True @rescaleFactor = 1.7 - %engineType = Raptor -} - -@PART[cryoengine-eagle-1]:FOR[RealismOverhaulEnginesPost] -{ - @title = Raptor (Vacuum Variant) - - @MODULE[ModuleEngineConfigs] - { - @configuration = Raptor Vacuum - !CONFIG[Raptor] {} - !CONFIG[Raptor?Non-Throttleable] {} - } + %engineType = RVac } //============= @@ -219,16 +197,6 @@ %engineTypeMult = 9 } -@PART[cryoengine-tyrannosaur-1]:FOR[RealismOverhaulEnginesPost] -{ - @title = Raptor (Surface Variant) - - @MODULE[ModuleEngineConfigs] - { - !CONFIG[Raptor?Vacuum] {} - } -} - //============= // BE-4 //============= @@ -305,7 +273,7 @@ %fuelCrossFeed = true %breakingForce = 10000 %breakingTorque = 10000 - + //fix node position @MODULE[ModuleB9PartSwitch] {