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//BE-4 engine | ||
//VSR | ||
// | ||
// http://www.spacelaunchreport.com/vulcan.html | ||
// | ||
//FIXME: stupendously preliminary config | ||
// ================================================== | ||
// BE-4 global engine configuration. | ||
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// Gross Mass: 2250 Kg | ||
// Throttle Range: 30% to 100% | ||
// O/F Ratio: 3.6 | ||
// Burn Time: 400 s (minimum) | ||
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// Sources: | ||
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// Blue Origin - BE-4 engine: https://www.blueorigin.com/be4 | ||
// United Launch Alliance - BE-4 rocket engine: http://www.ulalaunch.com/uploads/docs/BE-4_Fact_Sheet_Web_Final_2.pdf | ||
// Space Launch Report - Vulcan launch vehicle: http://www.spacelaunchreport.com/vulcan.html | ||
// NASASpaceFlight - IAF Blue Origin presentation: https://forum.nasaspaceflight.com/index.php?topic=10685.msg1665037#msg1665037 | ||
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// Used by: | ||
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// * Ven Stock Revamp | ||
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// Notes: | ||
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// * Stupendously preliminary config as no solid information about the operational parameters of the engine have been released yet. | ||
// * No TestFlight compatibility since this global engine config represents unflown hardware. | ||
// ================================================== | ||
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@PART[*]:HAS[#engineType[BE4]]:FOR[RealismOverhaulEngines] | ||
{ | ||
%category = Engine | ||
%title = BE-4 | ||
%manufacturer = Blue Origin | ||
%description = The BE-4 is an oxidizer-rich staged combustion engine that burns LNG/LOX. Though initially developed for use on a Blue Origin launch vehicle, in 2014 United Launch Alliance announced that their new Vulcan booster, the successor to the Atlas V and Delta IV, will be powered by a pair of BE-4 engines. | ||
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%description = The BE-4 is an oxidizer-rich staged combustion Methalox engine. Though initially developed for use on a Blue Origin launch vehicle, in 2014 United Launch Alliance announced that their new Vulcan launch vehicle, the successor to both the Atlas V and Delta IV launch vehicles, will be powered by a pair of BE-4 engines. Diameter: 2 m. | ||
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@MODULE[ModuleEngines*] | ||
{ | ||
%minThrust = 794.25 | ||
%maxThrust = 2647.5 | ||
%heatProduction = 100 | ||
%EngineType = LiquidFuel | ||
@useThrustCurve = False | ||
@useEngineResponseTime = False | ||
@engineAccelerationSpeed = 0 | ||
@engineDecelerationSpeed = 0 | ||
%ullage = True | ||
%pressureFed = False | ||
%ignitions = 4 | ||
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!IGNITOR_RESOURCE,*{} | ||
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!thrustCurve,*{} | ||
} | ||
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!MODULE[ModuleEngineConfigs],*{} | ||
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MODULE | ||
{ | ||
name = ModuleEngineConfigs | ||
type = ModuleEngines | ||
configuration = BE-4 | ||
modded = false | ||
origMass = 2.25 | ||
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CONFIG | ||
{ | ||
name = BE-4 | ||
minThrust = 794.25 | ||
maxThrust = 2647.5 | ||
minThrust = 1060 // Guess 40% throttle | ||
PROPELLANT // Guess MR = 3.25, typical for first-stage LNG/LOX | ||
{ | ||
name = LqdMethane | ||
ratio = 0.452 | ||
DrawGauge = true | ||
} | ||
PROPELLANT | ||
{ | ||
name = LqdOxygen | ||
ratio = 0.548 | ||
} | ||
atmosphereCurve // http://www.spacelaunchreport.com/vulcan.html, 2015-11-16, generally agrees with NasaSpaceflight.com L2 | ||
{ | ||
key = 0 335 | ||
key = 1 310 | ||
} | ||
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heatProduction = 100 | ||
massMult = 1.0 | ||
ullage = True | ||
pressureFed = False | ||
ignitions = 1 | ||
ignitions = 4 | ||
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IGNITOR_RESOURCE | ||
{ | ||
name = ElectricCharge | ||
amount = 0.5 | ||
} | ||
IGNITOR_RESOURCE | ||
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PROPELLANT | ||
{ | ||
name = TEATEB | ||
amount = 1.0 | ||
name = LqdMethane | ||
ratio = 0.4286 | ||
DrawGauge = True | ||
} | ||
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PROPELLANT | ||
{ | ||
name = LqdOxygen | ||
ratio = 0.5714 | ||
DrawGauge = False | ||
} | ||
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atmosphereCurve | ||
{ | ||
key = 0 341 | ||
key = 1 305 | ||
} | ||
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massMult = 1.0 | ||
} | ||
} | ||
@MODULE[ModuleGimbal] | ||
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@MODULE[ModuleGimbal],* | ||
{ | ||
%gimbalRange = 8 // Guess, same as RD-180 | ||
%useGimbalResponseSpeed = true | ||
@gimbalRange = 8.0 // Guess, same as RD-180. | ||
%useGimbalResponseSpeed = True | ||
%gimbalResponseSpeed = 16 | ||
} | ||
!MODULE[ModuleAlternator] | ||
{ | ||
} | ||
!RESOURCE[ElectricCharge] | ||
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!MODULE[ModuleAlternator],*{} | ||
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!RESOURCE,*{} | ||
} | ||
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// ================================================== | ||
// TestFlight compatibility. | ||
// ================================================== | ||
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@PART[*]:HAS[@MODULE[ModuleEngineConfigs]:HAS[@CONFIG[BE-4]],!MODULE[TestFlightInterop]]:BEFORE[zTestFlight] | ||
{ | ||
TESTFLIGHT | ||
{ | ||
name = BE-4 | ||
ratedBurnTime = 400 | ||
ignitionReliabilityStart = 0.98 | ||
ignitionReliabilityEnd = 0.995 | ||
cycleReliabilityStart = 0.98 | ||
cycleReliabilityEnd = 0.995 | ||
} | ||
} |
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155
GameData/RealismOverhaul/RO_SuggestedMods/KerbalAtomics/KerbalAtomics.cfg
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@PART[ntr-sc-25-1]:FOR[RealismOverhaul] // resized into BNTR; smaller than Nerva 1+2 | ||
{ | ||
%engineType = BNTR | ||
%RSSROConfig = True | ||
%category = Propulsion | ||
@mass = 2.27 | ||
@maxTemp = 573.15 | ||
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// https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20040182399.pdf ; 2004 presentation, with a 1.56m diameter BNTR | ||
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@MODEL,0 | ||
{ | ||
@scale = 0.6,0.6,0.6 | ||
} | ||
rescaleFactor = 1.0 | ||
@node_stack_top = 0.0, 1.394, 0.0, 0.0, 1.0, 0.0, 2 | ||
@node_stack_bottom = 0.0, -1.21848, 0.0, 0.0, -1.0, 0.0, 2 | ||
@node_attach = 0.0, 0, 0.0, 0.0, 1.0, 0.0, 2 | ||
@attachRules = 1,1,1,1,0 | ||
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!MODULE[ModuleEngines*] | ||
{ | ||
%heatProduction = 100 | ||
%minThrust = 66.72 | ||
%maxThrust = 66.72 | ||
%ullage = True | ||
%ignitions = 60 | ||
@PROPELLANT[LiquidFuel] | ||
{ | ||
name = LqdHydrogen | ||
ratio = 1.0 | ||
DrawGauge = True | ||
} | ||
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@PROPELLANT | ||
{ | ||
name = EnrichedUranium | ||
ratio = 1.0813e-15 | ||
DrawGauge = False | ||
ignoreForIsp = True | ||
} | ||
@atmosphereCurve | ||
{ | ||
@key,0 = 0 930 | ||
@key,1 = 1 380 | ||
} | ||
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} | ||
!MODULE[MultiModeEngine] {} | ||
!MODULE[ModuleActiveRadiator] {} | ||
!MODULE[ModuleAlternator] {} | ||
!MODULE[ModuleGenerator] {} | ||
} | ||
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@PART[ntr-sc-125-1]:FOR[RealismOverhaul] | ||
{ | ||
%engineType = NERVA | ||
%RSSROConfig = True | ||
%category = Propulsion | ||
@mass = 2.27 | ||
@maxTemp = 573.15 | ||
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@MODEL,0 | ||
{ | ||
@scale = 2.57,2.35,2.57 | ||
} | ||
rescaleFactor = 1.0 | ||
@node_stack_top = 0.0, 3.948, 0.0, 0.0, 1.0, 0.0, 1 | ||
@node_stack_bottom = 0.0, -6.23, 0.0, 0.0, -1.0, 0.0, 1 | ||
@node_attach = 0.0, 0, 0.0, 0.0, 1.0, 0.0, 2 | ||
@attachRules = 1,1,1,1,0 | ||
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!MODULE[ModuleEngines*] | ||
{ | ||
%heatProduction = 100 | ||
%minThrust = 0 | ||
%maxThrust = 334 | ||
%ullage = True | ||
%ignitions = 60 | ||
@PROPELLANT[LiquidFuel] | ||
{ | ||
name = LqdHydrogen | ||
ratio = 1.0 | ||
DrawGauge = True | ||
} | ||
@PROPELLANT | ||
{ | ||
name = EnrichedUranium | ||
ratio = 0.00000000001 | ||
} | ||
@atmosphereCurve | ||
{ | ||
key = 0 825 | ||
key = 1 380 | ||
} | ||
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} | ||
!MODULE[MultiModeEngine] {} | ||
!MODULE[ModuleActiveRadiator] {} | ||
!MODULE[ModuleAlternator] {} | ||
!MODULE[ModuleGenerator] {} | ||
} | ||
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@PART[ntr-sc-125-2]:FOR[RealismOverhaul] | ||
{ | ||
%engineType = NERVAII | ||
%RSSROConfig = True | ||
%category = Propulsion | ||
@mass = 2.27 | ||
@maxTemp = 573.15 | ||
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@MODEL,0 // arbitrary rescale; feels like it should be slightly 'fatter', even if smaller than nerva | ||
{ | ||
@scale = 3.9,4.7125,3.9 | ||
} | ||
rescaleFactor = 1.0 | ||
@node_stack_top = 0.0, 5.4194, 0.0, 0.0, 1.0, 0.0, 1 | ||
@node_stack_bottom = 0.0, -6.888, 0.0, 0.0, -1.0, 0.0, 1 | ||
@node_attach = 0.0, 0, 0.0, 0.0, 1.0, 0.0, 2 | ||
@attachRules = 1,1,1,1,0 | ||
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!MODULE[ModuleEngines*] | ||
{ | ||
%heatProduction = 100 | ||
%minThrust = 750 | ||
%maxThrust = 867 | ||
%ullage = True | ||
%ignitions = 60 | ||
@PROPELLANT | ||
{ | ||
name = LqdHydrogen | ||
ratio = 1.0 | ||
DrawGauge = True | ||
} | ||
@PROPELLANT | ||
{ | ||
name = EnrichedUranium | ||
ratio = 0.00000000001 | ||
} | ||
@atmosphereCurve | ||
{ | ||
key = 0 850 | ||
key = 1 380 | ||
} | ||
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} | ||
!MODULE[MultiModeEngine] {} | ||
!MODULE[ModuleActiveRadiator] {} | ||
!MODULE[ModuleAlternator] {} | ||
!MODULE[ModuleGenerator] {} | ||
} |
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