Create SR28_Config.cfg

GameData/RealismOverhaul/Engine_Configs/SR28_Config.cfg

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+//	==================================================
+//	SR-28-3
+//
+//	Manufacturer: JPL
+//
+//	=================================================================================
+//	SR-28-3
+//	ATS 1/2/3?
+//
+//	Dry Mass: 41.37 kg (loaded weight 860 lbs - expended weight)	[1]
+//	Thrust (SL): ??? kN
+//	Thrust (Vac): 27.06 kN (24.46 kN average)	[1]
+//	ISP: ??? SL / 278.0 Vac		[1]
+//	Burn Time: 45		total burn time, action time ~42.8 seconds	[1]
+//	Chamber Pressure: 1.79 MPa peak	[2]
+//	Propellant: PUPE	JPL-540 used polyurethane binder [3]
+//	Prop Ratio: N/A
+//	Throttle: N/A
+//	Nozzle Ratio: 35 [2]
+//	Ignitions: 1
+//	=================================================================================
+
+//	Sources:
+
+//	[1] https://apps.dtic.mil/sti/citations/tr/AD0802218
+//	[2] https://ntrs.nasa.gov/api/citations/19720026092/downloads/19720026092.pdf
+//	[3] https://ntrs.nasa.gov/api/citations/19680012396/downloads/19680012396.pdf
+
+//	Used by:
+
+//	Notes:
+
+//	-1 uses steel case, -3 uses titanium
+//	total expended mass 348.72 kg
+//	==================================================
+@PART[*]:HAS[#engineType[SR28]]:FOR[RealismOverhaulEngines]
+{
+	%title = #roSR28Title	//SR-28
+	%manufacturer = #roMfrJPL
+	%description = #roSR28Desc
+
+	@tags ^= :$: USA jpl jet propulsion laboratory sr28 sr-28 solid srm upper pupe
+
+	%specLevel = operational
+
+	@MODULE[ModuleEngines*]
+	{
+		%EngineType = SolidBooster
+		%allowShutdown = False
+		%throttleLocked = True
+		%exhaustDamage = True
+	}
+
+	!MODULE[ModuleEngineConfigs],*{}
+	!MODULE[ModuleAlternator],*{}
+	!RESOURCE,*{}
+	!MODULE[ModuleFuelTanks],*{}
+
+	!MODULE[ModuleGimbal],*{}
+
+	MODULE
+	{
+		name = ModuleFuelTanks
+		volume = 197.02
+		type = PUPE
+		basemass = -1
+		TANK
+		{
+			name = PUPE
+			amount = 197.02
+			maxAmount = 197.02
+		}
+	}
+
+	MODULE
+	{
+		name = ModuleEngineConfigs
+		type = ModuleEngines
+		configuration = SR-28-3
+		modded = false
+		origMass = 0.04137
+		CONFIG
+		{
+			name = SR-28-3
+			specLevel = operational
+			minThrust = 27.06
+			maxThrust = 27.06
+			heatProduction = 100
+			PROPELLANT
+			{
+				name = PUPE
+				ratio = 1.0
+				DrawGauge = True
+			}
+			atmosphereCurve
+			{
+				key = 0 278.0
+				key = 1 150
+			}
+			curveResource = PUPE
+			//Estimated from [1]
+			thrustCurve
+			{
+				key = 0 0.03 19 19
+				key = 0.03 0.6 11.57143 11.57143
+				key = 0.1 0.89 2.871429 2.871429
+				key = 0.15 0.97 0.9250003 0.9250003
+				key = 0.27 1 0.02499983 0.02499983
+				key = 0.52 0.95 -0.4333333 -0.4333333
+				key = 0.73 0.81 -0.8333334 -0.8333334
+				key = 0.89 0.65 -1.269231 -1.269231
+				key = 0.955 0.55 -2.880341 -2.880341
+				key = 1 0.36 -4.22222 -4.22222
+			}
+
+			//ATS-1: 1 flight, 0 failures
+			//ATS-3: 1 flight 0 failures
+			//Using Star-13E data I guess
+			TESTFLIGHT:NEEDS[TestLite|TestFlight]
+			{
+				ratedBurnTime = 45
+				ignitionReliabilityStart = 0.985849
+				ignitionReliabilityEnd = 0.997170
+				cycleReliabilityStart = 0.985849
+				cycleReliabilityEnd = 0.997170
+				isSolid = True
+			}
+		}
+	}
+}