-
Notifications
You must be signed in to change notification settings - Fork 279
Commit
This commit does not belong to any branch on this repository, and may belong to a fork outside of the repository.
Note: TQ-11 is a vernier engine with 4 chambers used in conjunction with a TQ-12 upperstage engine. The engine are separate.
- Loading branch information
1 parent
56ec1d4
commit 5e9f9cc
Showing
2 changed files
with
331 additions
and
0 deletions.
There are no files selected for viewing
101 changes: 101 additions & 0 deletions
101
GameData/RealismOverhaul/Engine_Configs/TQ11_Config.cfg
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,101 @@ | ||
// ================================================== | ||
// 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
230
GameData/RealismOverhaul/Engine_Configs/TQ12_Config.cfg
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,230 @@ | ||
// ================================================== | ||
// 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 | ||
} | ||
} | ||
} | ||
} |