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Restore TF configs for generic thrusters #2829

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Restore TF configs for generic thrusters #2829

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60 changes: 36 additions & 24 deletions GameData/RealismOverhaul/Engine_Configs/RCS_Config.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -415,56 +415,68 @@
//FIXME: This should probably be shown in PAW, similar to MERF
@description ^= :$: <b><color=red> RCS requires High-Pressure tanks to function.</color></b>
}
@PART[*]:HAS[~useRcsMass[True],#engineType[RCSGeneric]]:FOR[RealismOverhaulEngines]
@PART[*]:HAS[#engineType[RCSGeneric],@MODULE[ModuleEngines*]]:FOR[RealismOverhaulEngines]
{
//just tag generic thrusters, since TF doesn't apply to RCS
%useRCSTestFlightConfig = true
}
@PART[*]:HAS[~useRcsMass[?rue],#engineType[RCSGeneric]]:FOR[RealismOverhaulEngines]
{
@MODULE[ModuleEngineConfigs]:HAS[#type[ModuleRCS]]
{
-origMass = NULL
}
}
@PART[*]:HAS[#useRCSTestFlightConfig[True],!MODULE[TestFlightInterop]]:BEFORE[zTestFlight]:NEEDS[TestLite|TestFlight]
//these have to cover an incredibly wide range of thrusters over a wide era, so be pretty generous
@PART[*]:HAS[#useRCSTestFlightConfig[?rue],!MODULE[TestFlightInterop]]:BEFORE[zTestFlight]:NEEDS[TestLite|TestFlight]
{
!useRCSTestFlightConfig = NULL

//cold gas thrusters completely inert, only failures likely from valves during start/shutdown
TESTFLIGHT
{
name = ColdGasRCS
mainConfiguration = engineConfig = Helium,engineConfig = Nitrogen:ColdGasRCS
ratedBurnTime = 1200
ratedBurnTime = 36000 //10 hours
ignitionReliabilityStart = 0.98
ignitionReliabilityEnd = 0.999
ignitionReliabilityEnd = 0.9999
ignitionDynPresFailMultiplier = 0.1
cycleReliabilityStart = 0.98
cycleReliabilityEnd = 0.999
reliabilityDataRateMultiplier = 0.1
techTransfer = NitrousOxide,HTP,Hydrazine,Cavea-B,MMH+NTO,MMH+MON3,MMH+MON10,UDMH+NTO,Aerozine50+NTO:50
cycleReliabilityStart = 0.99
cycleReliabilityEnd = 1.0
reliabilityDataRateMultiplier = 7.8 //100 minutes to max du?
techTransfer = NitrousOxide,HTP,Hydrazine,ASCENT,Cavea-B,MMH+NTO,MMH+MON3,MMH+MON10,UDMH+NTO,Aerozine50+NTO,Kerosene+O2,Syntin+O2,Ethanol+O2,CH4+O2,H2+O2:20
}

//catalyst erosion and burnthroughs can occur, but are rare
//Once again, most failures due to valves during ignition
TESTFLIGHT
{
name = MonopropellantRCS
mainConfiguration = engineConfig = NitrousOxide,engineConfig = HTP,engineConfig = Hydrazine,engineConfig = Cavea-B:MonopropellantRCS
ratedBurnTime = 1200
ignitionReliabilityStart = 0.98
ignitionReliabilityEnd = 0.999
mainConfiguration = engineConfig = NitrousOxide,engineConfig = HTP,engineConfig = Hydrazine,engineConfig = Cavea-B:MonopropellantRCS,engineConfig = ASCENT:MonopropellantRCS
ratedBurnTime = 36000 //10 hours
ignitionReliabilityStart = 0.96
ignitionReliabilityEnd = 0.9995
ignitionDynPresFailMultiplier = 0.1
cycleReliabilityStart = 0.98
cycleReliabilityEnd = 0.999
reliabilityDataRateMultiplier = 0.1
techTransfer = Helium,Nitrogen,MMH+NTO,MMH+MON3,MMH+MON10,UDMH+NTO,Aerozine50+NTO:50
cycleReliabilityStart = 0.975
cycleReliabilityEnd = 0.9995
reliabilityDataRateMultiplier = 7.8 //100 minutes to max du?
techTransfer = Helium,Nitrogen,MMH+NTO,MMH+MON3,MMH+MON10,UDMH+NTO,Aerozine50+NTO,Kerosene+O2,Syntin+O2,Ethanol+O2,CH4+O2,H2+O2:20
}

//more valves, potential for hard start, more failure modes
//burnthrough failures can occur, but are unlikely
//Reference AJ10-Mid (first AJ10 with restarts) for start data, AJ10-190 (modern AJ10) for end data
TESTFLIGHT
{
name = BipropellantRCS
mainConfiguration = engineConfig = MMH+NTO,engineConfig = MMH+MON3,engineConfig = MMH+MON10,engineConfig = UDMH+NTO,engineConfig = Aerozine50+NTO:BipropellantRCS
ratedBurnTime = 1200
ignitionReliabilityStart = 0.98
ignitionReliabilityEnd = 0.999
mainConfiguration = engineConfig = MMH+NTO,engineConfig = MMH+MON3,engineConfig = MMH+MON10,engineConfig = UDMH+NTO,engineConfig = Aerozine50+NTO:BipropellantRCS,engineConfig = Kerosene+O2:BipropellantRCS,engineConfig = Syntin+O2:BipropellantRCS,engineConfig = Ethanol+O2:BipropellantRCS,engineConfig = CH4+O2:BipropellantRCS,engineConfig = H2+O2:BipropellantRCS
ratedBurnTime = 36000 //10 hours
ignitionReliabilityStart = 0.90
ignitionReliabilityEnd = 0.9994
ignitionDynPresFailMultiplier = 0.1
cycleReliabilityStart = 0.98
cycleReliabilityEnd = 0.999
reliabilityDataRateMultiplier = 0.1
techTransfer = Helium,Nitrogen,NitrousOxide,HTP,Hydrazine,Cavea-B:50
cycleReliabilityStart = 0.95
cycleReliabilityEnd = 0.9994
reliabilityDataRateMultiplier = 7.8 //100 minutes to max du?
techTransfer = Helium,Nitrogen,NitrousOxide,HTP,Hydrazine,ASCENT,Cavea-B:20
}
}