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GameData/RealismOverhaul/Engine_Configs/YF73_Config.cfg
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// ================================================== | ||
// YF-73 | ||
// | ||
// Manufacturer: AALPT | ||
// | ||
// ================================================================================= | ||
// YF-73 | ||
// Long March 3 | ||
// | ||
// Dry Mass: 245 kg [B] | ||
// Thrust (SL): ??? kN | ||
// Thrust(Vac): 44.43 kN [B] | ||
// ISP: 212? SL / 419.9 Vac [B] | ||
// Burn Time: 750 [B] | ||
// Chamber Pressure: 2.63 MPa [B] | ||
// Propellant: LOX / LH2 | ||
// Prop Ratio: 5.0 [B] | ||
// Throttle: N/A | ||
// Nozzle Ratio: 40 [3] | ||
// Ignitions: 2 [B] | ||
// ================================================================================= | ||
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// Sources: | ||
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// [1] http://lpre.de/kbhm/index.htm | ||
// [2] https://web.archive.org/web/20170621153836/http://www.b14643.de/Spacerockets_1/China/CZ-3/Description/Frame.htm | ||
// [3] https://web.archive.org/web/20150717192824/http://www.b14643.de/Spacerockets/Diverse/Asian_Rocket_engines/engines.htm | ||
// [4] http://www.braeunig.us/space/specs/lgmarch.htm | ||
// [5] http://www.globalsecurity.org/space/library/report/1999/lm3bchapter2.pdf | ||
// [6] http://www.globalsecurity.org/space/library/report/1999/lm2echapter2.pdf | ||
// [7] https://en.wikipedia.org/wiki/YF-73 | ||
// [8] https://forum.nasaspaceflight.com/index.php?topic=8447.msg1104075#msg1104075 | ||
// [9] http://astronautix.com/y/yf-73.html | ||
// [A] History of Liquid Propellant Rocket Engines | ||
// [B] 世界导弹与航天发动机大全 | ||
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// Used by: | ||
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// Notes: | ||
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// ================================================== | ||
@PART[*]:HAS[#engineType[YF73]]:FOR[RealismOverhaulEngines] | ||
{ | ||
%title = #roYF73Title //YF-73 | ||
%manufacturer = #roMfrAALPT | ||
%description = #roYF73Desc | ||
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@tags ^= :$: prc china aalpt yf73 yf-73 liquid pump upper lqdhydrogen lqdoxygen | ||
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%specLevel = operational | ||
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@MODULE[ModuleEngines*] | ||
{ | ||
%EngineType = LiquidFuel | ||
} | ||
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!MODULE[ModuleEngineConfigs],*{} | ||
!MODULE[ModuleAlternator],*{} | ||
!RESOURCE,*{} | ||
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@MODULE[ModuleGimbal] | ||
{ | ||
%gimbalRange = 24 //4-chambers with one-plane gimbal of 24 degrees | ||
%useGimbalResponseSpeed = true | ||
%gimbalResponseSpeed = 16 | ||
} | ||
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MODULE | ||
{ | ||
name = ModuleEngineConfigs | ||
type = ModuleEngines | ||
origMass = 0.245 | ||
modded = false | ||
configuration = YF-73 | ||
CONFIG | ||
{ | ||
name = YF-73 | ||
description = Used on 3rd stage of CZ-3 | ||
specLevel = operational | ||
minThrust = 44.43 | ||
maxThrust = 44.43 | ||
heatProduction = 100 | ||
ullage = True | ||
pressureFed = False | ||
ignitions = 2 | ||
massMult = 1.0 | ||
PROPELLANT | ||
{ | ||
name = LqdHydrogen | ||
ratio = 0.7631 | ||
DrawGauge = True | ||
} | ||
PROPELLANT | ||
{ | ||
name = LqdOxygen | ||
ratio = 0.2369 | ||
} | ||
atmosphereCurve | ||
{ | ||
key = 0 419.9 | ||
key = 1 212 | ||
} | ||
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//CZ-3: 13 flights, 3 failures (2 cycle, 1 restart) | ||
//2 ignitions per flight | ||
//13 ignitions, 0 failures | ||
//13 cycles, 2 failures (1 before restart, 1 after) | ||
//12 restarts, 1 failures | ||
TESTFLIGHT:NEEDS[TestLite|TestFlight] | ||
{ | ||
testedBurnTime = 1800 //hydrogen engines are pretty durable. We'll give this half an hour | ||
ratedBurnTime = 750 | ||
safeOverburn = true | ||
ignitionReliabilityStart = 0.932692 | ||
ignitionReliabilityEnd = 0.986538 | ||
ignitionDynPresFailMultiplier = 10.0 | ||
cycleReliabilityStart = 0.803571 | ||
cycleReliabilityEnd = 0.960714 | ||
} | ||
} | ||
} | ||
} |
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