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base repository: KSP-RO/RealismOverhaul
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head repository: KSP-RO/RealismOverhaul
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compare: 669bf830e6d0
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  • 2 commits
  • 2 files changed
  • 2 contributors

Commits on Oct 6, 2018

  1. RSB bugfixes

    PhineasFreak committed Oct 6, 2018
    Copy the full SHA
    f2b10c0 View commit details

Commits on Oct 13, 2018

  1. Merge pull request #1932 from PhineasFreak/RO-RSB-Atlas-V-bugfixes

    [Bug Fix] RSB Atlas V
    raidernick authored Oct 13, 2018
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    669bf83 View commit details
Original file line number Diff line number Diff line change
@@ -297,7 +297,7 @@
// Atlas V CCB nose cone.
// Dimensions: 3.81 m x 2.8 m
// Inert Mass: 415 Kg
// Inert Mass: 425 Kg
// ==================================================
@PART[RSBnosecone381]:FOR[RealismOverhaul]
@@ -308,7 +308,7 @@
@manufacturer = Orbital ATK
@description = A 3.8 meter aerodynamic nose cone for the Atlas V HLV.
@mass = 0.415
@mass = 0.425
@crashTolerance = 16
@breakingForce = 250
@breakingTorque = 250
@@ -353,6 +353,8 @@
{
%RSSROConfig = True
%node_stack_payload = 0.0, 4.455, 0.0, 0.0, 1.0, 0.0, 2
@title = Common Centaur
@manufacturer = United Launch Alliance (ULA)
@description = The second stage of an Atlas V. Contains the necessary avionics, communications and power supply for mission times of up to 6 hours.
@@ -364,10 +366,14 @@
@maxTemp = 673.15
%skinMaxTemp = 773.15
%vesselIcon = Probe
!ActivatesEvenIfDisconnected = NULL
!stagingIcon = NULL
!MODULE[ModuleDecouple],*{}
// Two sets of RCS thrusters for three axis control and ullage:
// Aerojet Rocketdyne MR-106J (40 N) for attitude control.
// Aerojet Rocketdyne MR-106K (27 N) ullage control.
// Eight Aerojet Rocketdyne MR-106J (40 N) for attitude control.
// Four Aerojet Rocketdyne MR-106K (27 N) for ullage control.
@MODULE[ModuleRCS*]
{
@@ -378,18 +384,18 @@
transformMultipliers
{
trf0 = 0.0935
trf1 = 0.0935
trf2 = 0.0935
trf3 = 0.0935
trf4 = 0.0935
trf5 = 0.0935
trf6 = 0.0935
trf7 = 0.0935
trf8 = 0.0631
trf9 = 0.0631
trf10 = 0.0631
trf11 = 0.0631
trf0 = 0.09346
trf1 = 0.09346
trf2 = 0.09346
trf3 = 0.09346
trf4 = 0.09346
trf5 = 0.09346
trf6 = 0.09346
trf7 = 0.09346
trf8 = 0.06308
trf9 = 0.06308
trf10 = 0.06308
trf11 = 0.06308
}
PROPELLANT
@@ -428,7 +434,6 @@
basemass = -1
// Centaur fuel and oxidizer mass 20830 Kg.
// Following masses calculated from a 5.5:1 mixture ratio:
// Centaur fuel mass 3204.6 Kg.
@@ -615,7 +620,7 @@
// Atlas V 500 series aft stub adapter.
// Dimensions: 3.81 m x 4.1 m
// Inert Mass: 1240 Kg
// Inert Mass: 1525 Kg
// ==================================================
@PART[RSBinterstageAtlasCentaur500]:FOR[RealismOverhaul]
@@ -626,7 +631,7 @@
@manufacturer = United Launch Alliance (ULA)
@description = The aft Centaur Interstage Adapter (CIA) for the Atlas V 500 series. Typically used with a 500 series Atlas V fairing base encapsulating the entire Centaur upper stage. Place this interstage first, then snap the 500 series fairing base onto the "gap".
@mass = 1.24
@mass = 1.525
@crashTolerance = 16
@breakingForce = 250
@breakingTorque = 250
@@ -643,7 +648,7 @@
// Atlas 500 series aft stub adapter (procedural).
// Dimensions: 3.81 m x 4.1 m
// Inert Mass: 1240 Kg
// Inert Mass: 1525 Kg
// ==================================================
@PART[RSBfairingAtlas500]FOR[RealismOverhaul]
@@ -655,7 +660,7 @@
@manufacturer = United Launch Alliance (ULA)
@description = The procedural fairing version of the aft Centaur Interstage Adapter (CIA) for the Atlas V 500 series. Typically used with a 500 series Atlas V fairing base encapsulating the entire Centaur upper stage. Place this interstage first, then snap the 500 series fairing base onto the "gap".
@mass = 1.24
@mass = 1.525
@crashTolerance = 16
@breakingForce = 250
@breakingTorque = 250
@@ -729,7 +734,7 @@
@name = HTPB
}
atmosphereCurve
@atmosphereCurve
{
@key,0 = 0 254
@key,1 = 1 160
Original file line number Diff line number Diff line change
@@ -1329,7 +1329,7 @@
%engineType = RD180
%engineTypeMult = 1
%massOffset = 0.5
%ignoreMass = True
%ignoreMass = False
@MODULE[ModuleEngines*]
{