Starliner Boring Crew Services Configs (#3010)

* Boring Crew Services Configs - BCS Configs - RS88 Config Update * Update RO_Starliner.cfg * Starliner BCS Update - Added Conformal Decal - Added Alternate Forward Heatshield - Added Multiadapter - Added three duplicate adapters for SLS, Saturn, and Vulcan to fit their appropriate rescale values * Updates and Corrections - Corrected RealAntenas to use the Ka Band - Changed the Forward Heatshield and Docking cover to LRSI skinTempTags - Moved Kerbalism Support to an ROKerbalism Pull (Found Here: KSP-RO/ROKerbalism#164) - Fixed Sources on RS88 Config
KSP-RO · Nov 18, 2024 · 65449b4 · 65449b4
1 parent b66997d
commit 65449b4
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diff --git a/GameData/RealismOverhaul/Engine_Configs/RS88_Config.cfg b/GameData/RealismOverhaul/Engine_Configs/RS88_Config.cfg
@@ -1,33 +1,33 @@
 //	==================================================
 //	RS-88
 //
-//	Manufacturer: Rocketdyne
+//	Manufacturer: Aerojet Rocketdyne
 //
 //	=================================================================================
 //	RS-88
 //	prototype
 //
-//	Dry Mass: 250 Kg
-//	Thrust (SL): 230.86 kN
-//	Thrust (Vac): 255.77 kN	[4]
-//	ISP: 222 SL / 244 Vac	[4]
+//	Dry Mass: 294.835 Kg (640 lbm)	[5]
+//	Thrust (SL): 230.863 kN (51.9 klbf)
+//	Thrust (Vac): 255.773 kN (57.5 klbf)	[5]
+//	ISP: 222 SL / 244 Vac	[5]
 //	Burn Time: ???
-//	Chamber Pressure: 4.45 MPa	[4]
+//	Chamber Pressure: 4.957 MPa (719 psi)	[5]
 //	Propellant: LOX / Ethanol75
-//	Prop Ratio: 1.49	[4]
-//	Throttle: N/A
-//	Nozzle Ratio: 7.04	[4]
+//	Prop Ratio: 1.49
+//	Throttle: 50% - 100%
+//	Nozzle Ratio: 15
 //	Ignitions: 1
 //	=================================================================================
 //	LAE
 //	CST-100
 //
 //	Dry Mass: 250 Kg
-//	Thrust (SL): 176.6 kN	[5],[6] assuming SL
-//	Thrust (Vac): 193.49 kN
+//	Thrust (SL): 176.6 kN	[4]
+//	Thrust (Vac): 193.49 kN	[4]
 //	ISP: 230 SL / 252 Vac	estimated with RPA
 //	Burn Time: ???
-//	Chamber Pressure: 4.45? MPa		same as RS-88?
+//	Chamber Pressure: 4.45? MPa		same as RS-88?	[4]
 //	Propellant: MON3 / MMH
 //	Prop Ratio: 1.65?
 //	Throttle: 100-75%?		"precise throttle control"
@@ -36,29 +36,35 @@
 //	=================================================================================
 
 //	Sources:
-//		[1]NTRS - RS-88 Pad Abort Demonstrator Thrust Chamber Assembly:					http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20050237017.pdf
-//		[2]Encyclopedia Astronautica - RS-88 engine:										http://astronautix.com/r/rs-88.html
-//		[3]Boeing - Design Considerations for a Commercial Crew Transportation System:		http://www.boeing.com/assets/pdf/defense-space/space/ccts/docs/Space_2011_Boeing.pdf
-//		[4]https://arc.aiaa.org/doi/epdf/10.2514/6.2005-4422
-//		[5]https://www.spaceflightinsider.com/organizations/boeing/launch-abort-engines-boeing-cst-100-starliner-undergo-testing/
-//		[6]https://www.americaspace.com/2014/08/08/aerojet-rocketdyne-completes-ccicap-work-with-boeings-cst-100-spacecraft/
+
+//		[1] NTRS - RS-88 Pad Abort Demonstrator Thrust Chamber Assembly:									http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20050237017.pdf
+//		[2] Encyclopedia Astronautica - RS-88 engine:														http://astronautix.com/r/rs-88.html
+//		[3] Boeing - Design Considerations for a Commercial Crew Transportation System:						http://www.boeing.com/assets/pdf/defense-space/space/ccts/docs/Space_2011_Boeing.pdf
+//		[4] Bantam Family of Aerojet Rocketdyne Commercial Rocket Engines:									https://arc.aiaa.org/doi/abs/10.2514/6.2013-5459
+//		[5] RS-88 Pad Abort Demonstrator Thrust Chamber Assembly Testing at Marshall Space Flight Center:	https://ntrs.nasa.gov/api/citations/20050237017/downloads/20050237017.pdf
+//		[6] https://arc.aiaa.org/doi/epdf/10.2514/6.2005-4422
+//		[7] https://www.spaceflightinsider.com/organizations/boeing/launch-abort-engines-boeing-cst-100-starliner-undergo-testing/
+//		[8] https://www.americaspace.com/2014/08/08/aerojet-rocketdyne-completes-ccicap-work-with-boeings-cst-100-spacecraft/
+
 
 //	Used by:
 //		CST-100 pack
 //		RLA
+//		BoringCrewServices
+
 
 //	FIXME:
-//		No sources for some values (inert mass, rated burn time and ignition count).
+//		No sources for some values (rated burn time and ignition count).
 //	==================================================
 
 @PART[*]:HAS[#engineType[RS88]]:FOR[RealismOverhaulEngines]
 {
 	%category = Engine
 	%title = #roRS88Title	//RS-88
-	%manufacturer = #roMfrRocketdyne
+	%manufacturer = #roMfrAerojetRocketdyne
 	%description = #roRS88Desc	//A high thrust pressure-fed hypergolic engine. Initially designed and built as a part of the NASA Bantam System Technology program, aiming for a low cost, high power propulsion system, it was later modified by Lockheed Martin for use as a launch abort engine. A derivative of the RS-88 is used by the Boeing CST-100 "Starliner" spacecraft for launch aborts under the name "Launch Abort Engine - LAE".
 
-	@tags ^= :$: USA rocketdyne rs88 lae liquid pressure-fed booster ethanol mmh lqdoxygen nto
+	@tags ^= :$: USA aerojet rocketdyne rs88 lae liquid pressure-fed booster ethanol mmh lqdoxygen nto
 
 	%specLevel = operational
 
@@ -77,50 +83,49 @@
 	{
 		name = ModuleEngineConfigs
 		type = ModuleEngines
-		configuration = RS-88
+		configuration = LAE
 		modded = False
 		origMass = 0.25
 
 		CONFIG
 		{
 			name = RS-88
-			specLevel = operational
-			maxThrust = 255.77
-			minThrust = 191.83
+			description = LOX/Ethanol powered engine using a Gas Generator Cycle.
+			specLevel = prototype
+			maxThrust = 255.773
+			minThrust = 127.8865
 			ullage = True
-			pressureFed = True
-			ignitions = 1
-
-			IGNITOR_RESOURCE
-			{
-				name = ElectricCharge
-				amount = 0.1
-			}
-
+			pressureFed = False
+			ignitions = 10
+			massMult = 1.567616
 			PROPELLANT
 			{
 				name = Ethanol75
 				ratio = 0.5236
 				DrawGauge = True
 			}
-
 			PROPELLANT
 			{
 				name = LqdOxygen
 				ratio = 0.4764
 				DrawGauge = False
 			}
-
 			atmosphereCurve
 			{
 				key = 0 244
 				key = 1 222
 			}
+			IGNITOR_RESOURCE
+			{
+				name = ElectricCharge
+				amount = 0.1
+			}
 		}
 
 		CONFIG
 		{
 			name = LAE
+			description = Hypergolic and Pressure Fed variant of the RS-88 for use as a Launch Abort Engine on Boeing's CST-100 Starliner.
 			specLevel = operational
 			minThrust = 145.12
 			maxThrust = 193.49
@@ -130,31 +135,34 @@
 			ignitions = 1
 			throttleResponseRate = 100
 
-			IGNITOR_RESOURCE
-			{
-				name = ElectricCharge
-				amount = 0.1
-			}
-
 			PROPELLANT
 			{
 				name = MMH
 				ratio = 0.4973
 				DrawGauge = True
 			}
-
 			PROPELLANT
 			{
 				name = MON3
 				ratio = 0.5027
 				DrawGauge = False
 			}
-
+			PROPELLANT
+			{
+				name = Helium
+				ratio = 10.0
+				DrawGauge = False
+			}
 			atmosphereCurve
 			{
 				key = 0 252
 				key = 1 230
 			}
+			IGNITOR_RESOURCE
+			{
+				name = ElectricCharge
+				amount = 0.1
+			}
 		}
 	}
 }