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Add XASR-2 config (#3015)
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Capkirk123 authored Nov 18, 2024
1 parent 65449b4 commit e33e021
Showing 1 changed file with 72 additions and 2 deletions.
74 changes: 72 additions & 2 deletions GameData/RealismOverhaul/Engine_Configs/Aerobee_Config.cfg
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// Ignitions: 1
// =================================================================================
// XASR-1
// Aerobee 100
// Aerobee 100, RTV-N-8a1
//
// Dry Mass: 10.4 Kg
// Thrust (SL): 11.565 kN
// Thrust (Vac): ??? kN
// ISP: 200 SL / 235.44 Vac
// Burn Time: 40
// Chamber Pressure: 2.28 MPa
// Propellant: IRNFA / Aniline-Furfuryl Alcohol mix (ANFA37)
// By mass: 62.6% Aniline, 37.4% Furfuryl. By Volume: 65% Aniline, 35% Furfuryl. Represent with Aniline37
// Prop Ratio: 2.56 4.35 seems obviously wrong, setting to 2.56 due to lack of any better source
// Throttle: N/A
// Nozzle Ratio: 5.1
// Ignitions: 1
// =================================================================================
// XASR-2
// RTV-N-10
// identical to XASR-1, but with helium pressurization
//
// Dry Mass: 10.4 Kg
// Thrust (SL): 11.565 kN
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}
}
CONFIG
{
// source for some: http://www.designation-systems.net/dusrm/n-2.html
// More info: http://rasaero.com/dloads/The%20Aerobee%20Sounding%20Rockets.pdf
name = XASR-2
description = Improved XASR-1 with helium pressurization to improve performance.
specLevel = operational
maxThrust = 13.7628
minThrust = 13.7628
heatProduction = 40
autoVariationScale = 1.25

PROPELLANT
{
name = ANFA37
ratio = 0.3660
DrawGauge = True
}
PROPELLANT
{
ratio = 0.6340
name = IRFNA-III
}

PROPELLANT
{
name = Helium
ratio = 34.2
ignoreForIsp = true
}
atmosphereCurve
{
// Calculated from known Pc, AR, sl Isp
key = 0 235.44
key = 1 200
}
massMult = 1.3

ullage = True
ignitions = 1
pressureFed = True

TESTFLIGHT:NEEDS[TestLite|TestFlight]
{
ratedBurnTime = 40
ignitionReliabilityStart = 0.95
ignitionReliabilityEnd = 0.98
cycleReliabilityStart = 0.95
cycleReliabilityEnd = 0.96

techTransfer = XASR-1,WAC-Corporal:50
}
}
CONFIG
{
name = AJ10-27
description = Developed as an upgrade to the XASR-1. Continued to be used until the 1980s for meteorlogical studies.
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cycleReliabilityStart = 0.95
cycleReliabilityEnd = 0.96

techTransfer = XASR-1,WAC-Corporal:50
techTransfer = XASR-2,XASR-1,WAC-Corporal:50
}
}
}
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