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F100 Pitch/Yaw balance beam nozzle
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add thrust vectoring F100
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Capkirk123 committed Mar 3, 2024
1 parent 83f59f1 commit 4237118
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// Exhaust Mixer: true
// Adjustable Nozzle: true
// =================================================================================
// F100-PW-229PYBBN
// 1993, F-15 ACTIVE
//
// Dry Mass: 1756 kg Guess
// Thrust (Dry): 79.2 kN
// Thrust (Wet): 129.4 kN
// SFC (Dry): 0.726 lb/lbf-hr
// Area: 0.29 m^2 //Compressor Area
// BPR: 0.36 //Bypass Ratio
// CPR: 32.0 //Compressor Pressure Ratio
// FPR: 3.8 //Fan Ratio
// Mdes: 0.9 M //Mach Design Point
// Tdes: 250 K //Temp Design Point
// eta_n: 0.7 //Efficiency at afterburner rear / nozzle entrance
// FHV: 22500000 J //Fuel heat of burning
// TIT: 1755 K //Combustion peak temp
// TAB: 2864* K //Afterburner peak temp
// maxT3: 1100 K //Turbine max temperature
// Exhaust Mixer: true
// Adjustable Nozzle: true
// =================================================================================
// F100-PW-229EEP
// 2009, F-16V Block 70
//
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%rate = 75.0
}
}

!MODULE[ModuleGimbal]{}
@MODULE[ModuleGimbal]
{
%gimbalRange = 20
%gimbalResponseSpeed = 16
%useGimbalResponseSpeed = true
}

MODULE
{
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exhaustMixer = True
adjustableNozzle = True
thrustUpperLimit = 220
gimbalRange = 0

// Engine fitting params
defaultTPR = 0.85
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exhaustMixer = True
adjustableNozzle = True
thrustUpperLimit = 220
gimbalRange = 0

// Engine fitting params
defaultTPR = 0.85
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exhaustMixer = True
adjustableNozzle = True
thrustUpperLimit = 260
gimbalRange = 0

// Engine fitting params
defaultTPR = 0.85
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}
}
CONFIG
{
name = F100-PW-229PYBBN
description = Modified F100 with thrust vectoring Pitch/Yaw Balance Beam Nozzle for the F-15 ACTIVE technology demonstrator. Temperature Mach limit at 15 km: 2.99.
specLevel = operational
massMult = 1.2178

Area = 0.29 //Compressor Area
BPR = 0.36 //Bypass Ratio
CPR = 32.0 //Compressor Pressure Ratio
FPR = 3.8 //Fan Ratio
Mdes = 0.9 //Mach Design Point
Tdes = 250 //Temp Design Point
eta_c = 0.95 //Efficiency at burner inlet
eta_t = 0.98 //Efficiency at burner exit
eta_n = 0.7 //Efficiency at afterburner rear / nozzle entrance
FHV = 22500000 //Fuel heat of burning (joules?)
TIT = 1755 //Combustion peak temp
TAB = 2864 //Afterburner temp?
maxT3 = 1100 //Turbine max temperature
exhaustMixer = True
adjustableNozzle = True
thrustUpperLimit = 260
gimbalRange = 20

// Engine fitting params
defaultTPR = 0.85
dryThrust = 79.2
wetThrust = 129.4
maxThrust = 129.4 //Just to let MEC know thrust
drySFC = 0.726
throttleResponseMultiplier = 1.0

PROPELLANT
{
name = Kerosene
ratio = 1.0
DrawGauge = True
}
}
CONFIG
{
name = F100-PW-229EEP
description = F100 Engine Enhancement Package, integrating technology from the F119 and F135 programs, as used in the F-16V Block 70. Temperature Mach limit at 15 km: 3.11.
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exhaustMixer = True
adjustableNozzle = True
thrustUpperLimit = 260
gimbalRange = 0

// Engine fitting params
defaultTPR = 0.85
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6 changes: 6 additions & 0 deletions GameData/RealismOverhaul/RO_DependentMods/RO_AJE.cfg
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scale = 1.6, 2.8, 1.6
}
MODULE
{
name = ModuleGimbal
gimbalTransformName = Gimbal
}
%engineType = F100
}
//F404-GE-402
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