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Updates and Corrections
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- Corrected RealAntenas to use the Ka Band
- Changed the Forward Heatshield and Docking cover to LRSI skinTempTags
- Moved Kerbalism Support to an ROKerbalism Pull (Found Here: KSP-RO/ROKerbalism#164)
- Fixed Sources on RS88 Config
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SkyPhoenix999 committed Nov 10, 2024
1 parent 7bcf838 commit 151dc21
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30 changes: 15 additions & 15 deletions GameData/RealismOverhaul/Engine_Configs/RS88_Config.cfg
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// RS-88
// prototype
//
// Dry Mass: 294.835 Kg (640 lbm)
// Dry Mass: 294.835 Kg (640 lbm) [5]
// Thrust (SL): 230.863 kN (51.9 klbf)
// Thrust (Vac): 255.773 kN (57.5 klbf)
// ISP: 222 SL / 244 Vac
// Thrust (Vac): 255.773 kN (57.5 klbf) [5]
// ISP: 222 SL / 244 Vac [5]
// Burn Time: ???
// Chamber Pressure: 4.957 MPa (719 psi)
// Chamber Pressure: 4.957 MPa (719 psi) [5]
// Propellant: LOX / Ethanol75
// Prop Ratio: 1.49
// Throttle: 50% - 100%
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// CST-100
//
// Dry Mass: 250 Kg
// Thrust (SL): 176.6 kN
// Thrust (Vac): 193.49 kN
// Thrust (SL): 176.6 kN [4]
// Thrust (Vac): 193.49 kN [4]
// ISP: 230 SL / 252 Vac estimated with RPA
// Burn Time: ???
// Chamber Pressure: 4.45? MPa same as RS-88?
// Chamber Pressure: 4.45? MPa same as RS-88? [4]
// Propellant: MON3 / MMH
// Prop Ratio: 1.65?
// Throttle: 100-75%? "precise throttle control"
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// Sources:

// NTRS - RS-88 Pad Abort Demonstrator Thrust Chamber Assembly: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20050237017.pdf
// Encyclopedia Astronautica - RS-88 engine: http://astronautix.com/r/rs-88.html
// Boeing - Design Considerations for a Commercial Crew Transportation System: http://www.boeing.com/assets/pdf/defense-space/space/ccts/docs/Space_2011_Boeing.pdf
// Bantam Family of Aerojet Rocketdyne Commercial Rocket Engines: https://cdn.discordapp.com/attachments/929499424760168559/1294294593063620618/Bantam_Family_of_Aerojet_Rocketdyne_Commercial_Rocket_Engines.pdf?ex=670a7d45&is=67092bc5&hm=f21ca64fe391ddf54bef2a2d1924b4d02e846b660365ff69f2fbafdf1ac301ac&
// RS-88 Pad Abort Demonstrator Thrust Chamber Assembly Testing at Marshall Space Flight Center: https://cdn.discordapp.com/attachments/929499424760168559/1294294593461817404/farr2005.pdf?ex=670a7d45&is=67092bc5&hm=925cfbcf0ee368b71f93e7d931e5730597835d32b66c38742e064135658a2492&
// https://arc.aiaa.org/doi/epdf/10.2514/6.2005-4422
// https://www.spaceflightinsider.com/organizations/boeing/launch-abort-engines-boeing-cst-100-starliner-undergo-testing/
// https://www.americaspace.com/2014/08/08/aerojet-rocketdyne-completes-ccicap-work-with-boeings-cst-100-spacecraft/
// [1] NTRS - RS-88 Pad Abort Demonstrator Thrust Chamber Assembly: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20050237017.pdf
// [2] Encyclopedia Astronautica - RS-88 engine: http://astronautix.com/r/rs-88.html
// [3] Boeing - Design Considerations for a Commercial Crew Transportation System: http://www.boeing.com/assets/pdf/defense-space/space/ccts/docs/Space_2011_Boeing.pdf
// [4] Bantam Family of Aerojet Rocketdyne Commercial Rocket Engines: https://arc.aiaa.org/doi/abs/10.2514/6.2013-5459
// [5] RS-88 Pad Abort Demonstrator Thrust Chamber Assembly Testing at Marshall Space Flight Center: https://ntrs.nasa.gov/api/citations/20050237017/downloads/20050237017.pdf
// [6] https://arc.aiaa.org/doi/epdf/10.2514/6.2005-4422
// [7] https://www.spaceflightinsider.com/organizations/boeing/launch-abort-engines-boeing-cst-100-starliner-undergo-testing/
// [8] https://www.americaspace.com/2014/08/08/aerojet-rocketdyne-completes-ccicap-work-with-boeings-cst-100-spacecraft/


// Used by:
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{
name = ModuleRealAntenna
antennaDiameter = 0.8 //Same as Orion because I cannot find any data
RFBand = K //Default to K-band
}
}
@PART[BCS_Centauri_CrewCapsule]:NEEDS[RealFuels]:AFTER[ROCapsules]
{
@description ^= :$: Supports a crew of 7 for 2 days.:
@mass -= 0.07
@MODULE[ModuleFuelTanks]
{
// 7 Crew for 2 Days, Tanks filled for 4 people for ~4 Days
@volume = 460
TANK
{
name = Food
amount = 100
maxAmount = 100
}
TANK
{
name = Water
amount = 67
maxAmount = 67
}
TANK
{
name = Oxygen
amount = 10000
maxAmount = 10000
}
TANK
{
name = Nitrogen
amount = 200
maxAmount = 200
}
TANK
{
name = Waste
amount = 0
maxAmount = 9.32
}
TANK
{
name = WasteWater
amount = 0
maxAmount = 34.47
}
}
}
@PART[BCS_Centauri_CrewCapsule]:NEEDS[ProfileRealismOverhaul]:AFTER[RealismOverhaul]
{
%capsuleScrubbers = true
%scrubberCapacity = 2
%capsuleOrigin = US
@MODULE[ModuleCommand]
{
@RESOURCE[ElectricCharge]
{
@rate = 0.600 //Remove Climatization and LS power draw
}
}
MODULE
{
name = ProcessController
resource = _PressureControl
title = N2 Pressure Controller
desc = Use <b>Nitrogen</b> to maintain the internal atmosphere at a comfortable pressure.
capacity = 2
toggle = true
running = true
}
@MODULE[ProcessController],*
{
@capacity *= #$/CrewCapacity$
RFBand = Ka //Default to Ka-band
}
}
@PART[BCS_Centauri_CrewCapsule]:AFTER[RealismOverhaul_Materials]
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@title = CST-100 Docking Port Cover
@manufacturer = #roMfrBoeing
@description = A hingable cover for the NASA Docking System port on the front end of Boeing's Starliner capsule, designed to shield the docking port when not attached to the Space Station.
%skinTempTag = HRSI
%skinTempTag = LRSI
%internalTempTag = Instruments
%skinInsulationTag = True
}
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@description = Aerocover for Starliner's Parachutes, detach after re-entry to deploy the parachutes. Comes with a jettisonable nose cover to protect the forward section and docking port during launch.
@mass = 0.1
%ROSAFRescale = 1.6
%skinTempTag = HRSI
%skinTempTag = LRSI
%internalTempTag = Instruments
%skinInsulationTag = True
}
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@manufacturer = #roMfrBoeing
@description = Aerocover for Starliner's Parachutes, detach after re-entry to deploy the parachutes. Variant without the jettisonable nose cover.
@mass = 0.1
%skinTempTag = HRSI
%skinTempTag = LRSI
%internalTempTag = Instruments
%skinInsulationTag = True
}
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