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TQ-11 and TQ-12 Configs (#3005)
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Note: TQ-11 is a vernier engine with 4 chambers used in conjunction with a TQ-12 upperstage engine. The engine are separate.
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SkyPhoenix999 authored Oct 19, 2024
1 parent 56ec1d4 commit 5e9f9cc
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101 changes: 101 additions & 0 deletions GameData/RealismOverhaul/Engine_Configs/TQ11_Config.cfg
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// ==================================================
// TQ-11
//
// Manufacturer: LandSpace
//
// =================================================================================
// TQ-11
// Zhuque-2 (ZQ-2)
//
// Dry Mass: ??? Kg
// Thrust (SL): ??? kN
// Thrust (Vac): 80 kN
// ISP: 284.5 SL / 316.35 Vac
// Chamber Pressure: 10.1 MPa
// Propellant: LOX / CH4
// Prop Ratio: 2.92
// Ignitions: 4?
// =================================================================================
//
// Sources:
//
// https://www.landspace.com/engine/show.php?id=128
// https://www.thespacereview.com/article/3787/1
// https://en.wikipedia.org/wiki/TQ-11
// https://spacenews.com/space-pioneer-raises-14-million-to-develop-green-liquid-rocket-engines/
//
// Used by:
//
// KODS
//
// ==================================================

@PART[*]:HAS[#engineType[TQ11]]:FOR[RealismOverhaulEngines]
{
%category = Engine
%title = TQ-11
%manufacturer = #roMfrLS
%description = The TQ-11 is a Liquid Methane and Liquid Oxygen engine developed by LandSpace. Made up of 4 small nozzles, the engine serves as gimbal control for the Zhuque-2 2nd stage in conjunction with a TQ-12 Vacuum Engine. This engine is planned to be superceeded by the TQ-15A rocket engine on the Zhuque-2 Rocket. Powered by a Gas-Generator cycle, the TQ-11 powered the first Liquid Methane rocket to reach Earth Orbit.

@tags ^= :$: USA landspace tq11 zhuque liquid pump booster lqdmethane lqdoxygen

%specLevel = operational

@MODULE[ModuleEngines*]
{
%EngineType = LiquidFuel
}

!MODULE[ModuleEngineConfigs],*{}
!MODULE[ModuleAlternator],*{}
!RESOURCE,*{}

@MODULE[ModuleGimbal],*
{
@gimbalRange = 5 // Guess
%useGimbalResponseSpeed = True
%gimbalResponseSpeed = 16
}

MODULE
{
name = ModuleEngineConfigs
type = ModuleEngines
configuration = TQ-11
origMass = 0.2 // Guess
CONFIG
{
name = TQ-11
specLevel = operational
minThrust = 80
maxThrust = 80
heatProduction = 100
massMult = 1.0
ullage = True
pressureFed = False
ignitions = 4 // Guess

PROPELLANT
{
name = LqdMethane
ratio = 0.48196
DrawGauge = True
}
PROPELLANT
{
name = LqdOxygen
ratio = 0.51804
}
IGNITOR_RESOURCE
{
name = ElectricCharge
amount = 0.5
}
atmosphereCurve
{
key = 0 337
key = 1 200 // Guess
}
}
}
}
230 changes: 230 additions & 0 deletions GameData/RealismOverhaul/Engine_Configs/TQ12_Config.cfg
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// ==================================================
// TQ-12
//
// Manufacturer: LandSpace
//
// =================================================================================
// TQ-12
// Zhuque-2 (ZQ-2)
//
// Dry Mass: 470 Kg // Guess
// Thrust (SL): 670 kN
// Thrust (Vac): 745 kN
// ISP: 284.5 SL / 316.35 Vac
// Chamber Pressure: 10.1 MPa
// Propellant: LOX / CH4
// Prop Ratio: 2.92
// Ignitions: 4?
// =================================================================================
// TQ-12A
// Zhuque-2 (ZQ-2)
//
// Dry Mass: 370 Kg // Guess (w/ 100kg reducation)
// Thrust (SL): 730.3 kN
// Thrust (Vac): 812.05 kN
// ISP: 284.5 SL / 316.35 Vac
// Chamber Pressure: 10.1 MPa
// Propellant: LOX / CH4
// Prop Ratio: 2.92
// Ignitions: 4?
// =================================================================================
// TQ-12V
// Zhuque-3 (ZQ-3)
//
// Dry Mass: 517 Kg // Guess
// Thrust (SL): ??? kN
// Thrust (Vac): 785 kN
// ISP: ??? SL / 337 Vac
// Chamber Pressure: 10.1 MPa
// Propellant: LOX / CH4
// Prop Ratio: 2.92
// Ignitions: 4?
// =================================================================================
//
// Sources:
//
// https://mp.weixin.qq.com/s/epm849_1t18X8WCQbuWRjA
// https://mp.weixin.qq.com/s?__biz=MzA5OTQ3OTA1NA==&mid=2653170924&idx=1&sn=def945de793bfa71aacf2c48bba3c73f&chksm=8b51378dbc26be9b15c22375488d3015bebc23467099e86667b739b02252bfadddb2056ba19b&token=575113164&lang=zh_CN&scene=21#wechat_redirect
// https://en.wikipedia.org/wiki/TQ-12
//
// Used by:
//
// KODS
//
// ==================================================

@PART[*]:HAS[#engineType[TQ12]]:FOR[RealismOverhaulEngines]
{
%category = Engine
%title = TQ-12
%manufacturer = #roMfrLS
%description = The TQ-12 is a Liquid Methane and Liquid Oxygen engine developed by LandSpace. Four of these engines are used on the Zhuque-2 (ZQ-2) Launch Vehicle, and 9 are used on the Zhuque-3 (ZQ-3) rocket's 1st Stage, a Vacuum variant also powers the 2nd stage of the Zhuque-3. Powered by a Gas-Generator cycle, the TQ-12 powered the first Liquid Methane rocket to reach Earth Orbit.
@tags ^= :$: USA landspace tq12 zhuque liquid pump booster lqdmethane lqdoxygen
%specLevel = operational
@MODULE[ModuleEngines*]
{
%EngineType = LiquidFuel
}
!MODULE[ModuleEngineConfigs],*{}
!MODULE[ModuleAlternator],*{}
!RESOURCE,*{}
@MODULE[ModuleGimbal],*
{
@gimbalRange = 5 // Guess
%useGimbalResponseSpeed = True
%gimbalResponseSpeed = 16
}
MODULE
{
name = ModuleEngineConfigs
type = ModuleEngines
configuration = TQ-12
origMass = 0.47 // Best Guess
CONFIG
{
name = TQ-12
description = Base version of the engine used on the Zhuque-2 Launch Vehicle
specLevel = operational
minThrust = 338.636 // 45% throttle range
maxThrust = 745
heatProduction = 100
massMult = 1.0
ullage = True
pressureFed = False
ignitions = 4 // Guess
PROPELLANT
{
name = LqdMethane
ratio = 0.48196
DrawGauge = True
}
PROPELLANT
{
name = LqdOxygen
ratio = 0.51804
}
IGNITOR_RESOURCE
{
name = ElectricCharge
amount = 0.5
}
atmosphereCurve
{
key = 0 316.35
key = 1 284.5
}
}
CONFIG
{
name = TQ-12A
description = Upgraded Engine with 9% higher thrust and 100kg decrease in dry mass
specLevel = prototype
minThrust = 365.42 // 45% throttle range
maxThrust = 812.05
heatProduction = 100
massMult = 0.787 // 100kg Decrease
ullage = True
pressureFed = False
ignitions = 4 // Guess
PROPELLANT
{
name = LqdMethane
ratio = 0.48196
DrawGauge = True
}
PROPELLANT
{
name = LqdOxygen
ratio = 0.51804
}
IGNITOR_RESOURCE
{
name = ElectricCharge
amount = 0.5
}
atmosphereCurve
{
key = 0 316.35
key = 1 284.5
}
}
CONFIG
{
name = TQ-12-V
description = Vacuum Version for use on the Zhuque-3 Launch Vehicle
specLevel = operational
minThrust = 353.25 // 45% throttle range
maxThrust = 785
heatProduction = 100
massMult = 1.1
ullage = True
pressureFed = False
ignitions = 4 // Guess
PROPELLANT
{
name = LqdMethane
ratio = 0.48196
DrawGauge = True
}
PROPELLANT
{
name = LqdOxygen
ratio = 0.51804
}
IGNITOR_RESOURCE
{
name = ElectricCharge
amount = 0.5
}
atmosphereCurve
{
key = 0 337
key = 1 200 // Guess
}
}
CONFIG
{
name = TQ-12A-V
description = Upgraded Engine with 9% higher thrust and 100kg decrease in dry mass
specLevel = operational
minThrust = 385.0425 // 45% throttle range
maxThrust = 855.65
heatProduction = 100
massMult = 0.887 // 100kg Decrease
ullage = True
pressureFed = False
ignitions = 4 // Guess
PROPELLANT
{
name = LqdMethane
ratio = 0.48196
DrawGauge = True
}
PROPELLANT
{
name = LqdOxygen
ratio = 0.51804
}
IGNITOR_RESOURCE
{
name = ElectricCharge
amount = 0.5
}
atmosphereCurve
{
key = 0 337
key = 1 200 // Guess
}
}
}
}

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