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  • 8 commits
  • 4 files changed
  • 2 contributors

Commits on Jul 8, 2018

  1. ICPS and EUS fix

    DocRockwell authored Jul 8, 2018
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Commits on Jul 10, 2018

  1. Update SSTU_Orion.cfg

    DocRockwell authored Jul 10, 2018
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Commits on Sep 29, 2018

  1. Merge pull request #1910 from DocRockwell/ICPS-and-EUS-fix

    SSTU ICPS and EUS fix
    raidernick authored Sep 29, 2018
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195 changes: 151 additions & 44 deletions GameData/RealismOverhaul/RO_SuggestedMods/SSTU/SSTU_Orion.cfg
Original file line number Diff line number Diff line change
@@ -959,9 +959,12 @@
//**********************************************************
// Exploration Upper Stage
//**********************************************************
@PART[SSTU-SC-C-HUS]:AFTER[SSTU]
@PART[SSTU-SC-C-HUS]:FOR[RealismOverhaul]:NEEDS[SSTU]
{
%RSSROConfig = True
%engineType = RL10
//%useRcsConfig = RCSBlock
%ignoreMass = true
@MODEL,0
{
@@ -1024,18 +1027,21 @@
!RESOURCE,* {}
MODULE
{
name = ModuleFuelTanks
type = ServiceModule
volume = 647
basemass = -1
TANK
{
name = Hydrazine
amount = 647
maxAmount = 647
name = ModuleCommand
minimumCrew = 0
hasHibernation = False
RESOURCE
{
name = ElectricCharge
rate = 0.3
varyTime = False
useSI = True
displayUnitMult = 1000
unitName = Watts
}
}
}
MODULE
{
name = ModuleFuelTanks
@@ -1047,18 +1053,35 @@
{
name = LqdHydrogen
amount = 265423.9732626
maxAmount = 265423.9732626
maxAmount = 272254.6
}
TANK
{
name = LqdOxygen
amount = 96830.6647374
maxAmount = 96830.6647374
amount = 90000
maxAmount = 90000
}
TANK
{
name = Hydrazine
amount = 647
maxAmount = 647
}
TANK
{
name = ElectricCharge
amount = 10800
maxAmount = 10800
}
}
%engineType = RL10
%ignoreMass = true
MODULE
{
name = ModuleFuelTanks
type = ServiceModule
volume = 647
basemass = -1
}
@MODULE[ModuleEnginesFX]
{
@@ -1078,7 +1101,7 @@
{
%maxTopDiameter = 20
%maxBottomDiameter = 20
%topDiameterIncrement = 0.5
%topDiameterIncrement = 0.2
!FAIRING {}
FAIRING
{
@@ -1090,6 +1113,22 @@
}
}
@MODULE[SSTUNodeFairing],1
{
%maxTopDiameter = 20
%maxBottomDiameter = 20
%bottomDiameterIncrement = 0.2
!FAIRING {}
FAIRING
{
topY = 1.086288
bottomY = -8.48450454554
topRadius = 4.2
bottomRadius = 4.2
canAdjustBottom = true
}
}
@MODULE[SSTUModelConstraint]
{
@LOOK_CONST,0
@@ -1127,7 +1166,7 @@
@MODULE[SSTUAnimateEngineHeat]
{
@meshName = SC-ENG-RL10A-3
@engineID = RL10A-3
@engineID = RL10A-1
}
@MODULE[SSTUSelectableNodes]
@@ -1140,7 +1179,7 @@
{
name = ModuleRCS
thrusterTransformName = SC-GEN-RCS-4F-T-ThrustTransform
thrusterPower = 0.275
thrusterPower = 0.400
resourceFlowMode = STAGE_PRIORITY_FLOW
enableRoll = true
enableYaw = true
@@ -1169,7 +1208,7 @@
%MODULE[ModuleRTAntennaPassive]:NEEDS[RemoteTech]
{
%TechRequired = unmannedTech
%OmniRange = 300000
%OmniRange = 5000000
%TRANSMITTER
{
@@ -1179,24 +1218,39 @@
}
}
}
@PART[SSTU-SC-C-HUS]:AFTER[RealismOverhaulEngines]
@PART[SSTU-SC-C-HUS]:AFTER[RealismOverhaulEngines]:NEEDS[SSTU]
{
@title = Exploration Upper Stage
%manufacturer = Boeing
%description = The Exploration Upper Stage (EUS) for the Space Launch System Blocks IB and II. It is a heavy upper stage designed to propel the larger payloads of the later SLS blocks.
@MODULE[ModuleEngineConfigs]
@MODULE[ModuleEngineConfigs]
{
!CONFIG,*:HAS[~name[RL10C-1]] {}
!CONFIG[RL10A-1] {}
!CONFIG[RL10A-3-1] {}
!CONFIG[RL10A-3-3] {}
!CONFIG[RL10A-3-3A] {}
!CONFIG[RL10A-5] {}
!CONFIG[RL10B-2] {}
!CONFIG[RL10A-4] {}
!CONFIG[RL10A-4-1-2] {}
@CONFIG[*],*
{
@minThrust *= 4
@maxThrust *= 4
}
}
}
//**********************************************************
// Interim Cryogenic Propulsion Stage
//**********************************************************
@PART[SSTU-SC-C-ICPS]:AFTER[SSTU]
@PART[SSTU-SC-C-ICPS]:FOR[RealismOverhaul]:NEEDS[SSTU]
{
%RSSROConfig = True
%engineType = RL10
//%useRcsConfig = RCSBlock
%ignoreMass = true
@MODEL,*
{
@@ -1221,6 +1275,7 @@
@MODEL,5
{
%position = 0, -4.1841, 0
%scale = 1.6967,1.6967,1.6967
}
@node_stack_bottom = 0,-5.99504,0,0,-1,0,5
@node_stack_top = 0,3.32604,0,0,1,0,5
@@ -1229,46 +1284,98 @@
@tags ^=:$:, orion, icps, sstu, interim, upper, stage, sls, delta
@mass = 3.66 //estimate just under 5% heavier than standard 5 m DCSS
@mass = 3.49 //estimate just under 5% heavier than standard 5 m DCSS
!RESOURCE,* {}
MODULE
{
name = ModuleCommand
minimumCrew = 0
hasHibernation = False
RESOURCE
{
name = ElectricCharge
rate = 0.3
varyTime = False
useSI = True
displayUnitMult = 1000
unitName = Watts
}
}
MODULE
{
name = ModuleFuelTanks
type = ServiceModule
volume = 226
type = Cryogenic
volume = 94900
basemass = -1
TANK
{
name = LqdHydrogen
amount = 69900
maxAmount = 69900 //74534 // Approx 30% increase in LH2 tank length
}
TANK
{
name = LqdOxygen
amount = 25000
maxAmount = 25000 //20366
}
TANK
{
name = Hydrazine
amount = 226
maxAmount = 226
}
TANK
{
name = ElectricCharge
amount = 10800
maxAmount = 10800
}
}
MODULE
{
name = ModuleFuelTanks
type = Cryogenic
volume = 94900
type = ServiceModule
volume = 226
basemass = -1
TANK
}
@MODULE[ModuleEnginesFX]
{
//runningEffectName = running_closed
//thrustVectorTransformName = RL10B-2-ThrustTransform
@minThrust = 110
@maxThrust = 110
@heatProduction = 100
!PROPELLANT[*],* {}
!atmosphereCurve,* {}
PROPELLANT
{
name = LqdHydrogen
amount = 55820
maxAmount = 74534 // Approx 30% increase in LH2 tank length
ratio = 0.7325
DrawGauge = True
}
TANK
PROPELLANT
{
name = LqdOxygen
amount = 20366
maxAmount = 20366
ratio = 0.2675 //5.88
}
atmosphereCurve
{
key = 0 465.5
key = 1 235
}
%ullage = True
%ignitions = 15
%IGNITOR_RESOURCE
{
%name = ElectricCharge
%amount = 0.5
}
}
%engineType = RL10
%ignoreMass = true
@MODULE[ModuleGimbal]
{
@gimbalRange = 6
@@ -1311,7 +1418,7 @@
{
%maxTopDiameter = 10
%maxBottomDiameter = 10
%topDiameterIncrement = 0.5
%topDiameterIncrement = 0.2
!FAIRING {}
FAIRING
{
@@ -1327,14 +1434,14 @@
{
%maxTopDiameter = 10
%maxBottomDiameter = 10
%bottomDiameterIncrement = 0.5
%bottomDiameterIncrement = 0.2
!FAIRING {}
FAIRING
{
topY = -0.05882665196
bottomY = -8.48450454554
topRadius = 2.5
bottomRadius = 4.2
bottomRadius = 2.5
canAdjustBottom = true
}
}
@@ -1348,7 +1455,7 @@
%MODULE[ModuleRTAntennaPassive]:NEEDS[RemoteTech]
{
%TechRequired = unmannedTech
%OmniRange = 300000
%OmniRange = 5000000
%TRANSMITTER
{
@@ -1358,13 +1465,13 @@
}
}
}
@PART[SSTU-SC-C-ICPS]:AFTER[RealismOverhaulEngines]
@PART[SSTU-SC-C-ICPS]:AFTER[RealismOverhaulEngines]:NEEDS[SSTU]
{
@title = Interim Cryogenic Propulsion Stage (ICPS)
%manufacturer = Boeing
%description = The Interim Cryogenic Propulsion Stage (ICPS) consists of a modified Delta IV 5 m upper stage. Its structure has been strengthened to support SLS flight loads and the hydrogen tank has been stretched by 46 cm to account for on-orbit boiloff. //http://forum.nasaspaceflight.com/index.php?topic=35528.320
@MODULE[ModuleEngineConfigs]
@MODULE[ModuleEngineConfigs]
{
!CONFIG,*:HAS[~name[RL10B-2]] {}
}
Original file line number Diff line number Diff line change
@@ -16,13 +16,13 @@
PLUME
{
name = Hydrolox-Upper
transformName = RL10B-2-ThrustTransform
transformName = RL10A-3-ThrustTransform
localRotation = 0,0,0
localPosition = 0,0,2.7
fixedScale = 2.1
localPosition = 0,0,1.3
fixedScale = 1.6
energy = 1
speed = 1.0
emissionMult = 1.5
speed = 1.2
emissionMult = 0.5
}
}

Original file line number Diff line number Diff line change
@@ -18,11 +18,13 @@
name = Hydrolox-Upper
transformName = RL10B-2-ThrustTransform
localRotation = 0,0,0
localPosition = 0,0,2.7
fixedScale = 2.1
flarePosition = 0,0,2.3
flareScale = 1.9
plumePosition = 0,0,2.7
plumeScale = 1.9
energy = 1
speed = 1.0
emissionMult = 1.5
speed = 1.2
emissionMult = 0.5
}
}

Original file line number Diff line number Diff line change
@@ -18,9 +18,9 @@
name = Hydrolox-Upper
transformName = RL10B-2-ThrustTransform
localRotation = 0,0,0
plumePosition = 0,0,2.0
plumeScale = 2
flarePosition = 0,0,2.3
plumePosition = 0,0,2.3
plumeScale = 1.9
flarePosition = 0,0,2.8
flareScale = 1.9
energy = 1
speed = 1.2