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Showing 9 changed files with 81 additions and 964 deletions.
18 changes: 17 additions & 1 deletion GameData/RealismOverhaul/Engine_Configs/GEM40_Config.cfg
Original file line number Diff line number Diff line change
@@ -6,6 +6,22 @@
@title = GEM 40
%manufacturer = Hercules
@description = The Graphite-Epoxy Motor (GEM) replaced the steel case used on earlier Castor-series boosters with a lighter composite case. The 40-inch (1-meter) diameter GEM 40 was used on the Delta II 7000-series in sets of three, four, or nine. When nine boosters were used, six were ignited at liftoff and the remaining three were ignited after burnout and jettison of the first six. Burn time: 58 seconds. Diameter: [1.02 m].

!RESOURCE,*{}

MODULE
{
name = ModuleFuelTanks
volume = 6647.45762712
type = HTPB
basemass = -1
TANK
{
name = HTPB
amount = 6647.45762712
maxAmount = 6647.45762712
}
}

MODULE
{
@@ -182,5 +198,5 @@
key = 0.0015 0.25
}
}
}
}
}
16 changes: 16 additions & 0 deletions GameData/RealismOverhaul/Engine_Configs/GEM46_Config.cfg
Original file line number Diff line number Diff line change
@@ -7,6 +7,22 @@
@title = GEM 46
%manufacturer = ATK
@description = The 46-inch (1.2-meter) diameter GEM 46 was used on the Delta III and Delta II Heavy. On both vehicles they were used in sets of nine, with six ignited at liftoff and three ignited after burnout of the first six. On the Delta III, three ground-lit boosters were equipped with thrust vector control (TVC) while all the remaining boosters used fixed nozzles. The Delta II Heavy used no boosters with TVC. Burn time 75 seconds. Diameter: [1.17 m].

!RESOURCE,*{}

MODULE
{
name = ModuleFuelTanks
volume = 9528.0022
type = HTPB
basemass = -1
TANK
{
name = HTPB
amount = 9528.0022
maxAmount = 9528.0022
}
}

MODULE
{
64 changes: 41 additions & 23 deletions GameData/RealismOverhaul/Engine_Configs/GEM60_Config.cfg
Original file line number Diff line number Diff line change
@@ -1,20 +1,20 @@
// ==================================================
// GEM 60 solid rocket motor global engine configuration.

// Throttle Range: N/A
// Burn Time: 90 s
// O/F Ratio: 2.12

// Sources:

// Orbital ATK Space Propulsion Products Catalog (2012): https://www.orbitalatk.com/flight-systems/propulsion-systems/launch-abort-motor/docs/orbital_atk_motor_catalog_(2012).pdf
// Encyclopedia Astronautica - GEM 60: http://www.astronautix.com/g/gem60.html

// Used by:

//
// ATK GEM-60 Brochure: http://www.alternatewars.com/BBOW/Space_Engines/GEM-60.pdf
// Orbital ATK Space Propulsion Catalog (2012).pdf
//
// Dimensions: 1.52 m x 16.2 m
// Gross Mass: 33200 Kg (w/o TVC), 33800 Kg (w/ TVC)
// Max Thrust: 1235.947
// ISP: 274
// Burn Time: 90.8s
// Gimbal: 5 degrees
//
// CMES
// KW Rocketry
// Real Scale Boosters
// Bluedog_DB
// ==================================================

@PART[*]:HAS[#engineType[GEM-60]]:FOR[RealismOverhaulEngines]
@@ -31,26 +31,48 @@

@MODULE[ModuleGimbal]
{
@gimbalRange = 5.0
@gimbalRange = 4.0
%useGimbalResponseSpeed = True
%gimbalResponseSpeed = 16
}

!MODULE[ModuleEngineConfigs],*{}

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

!MODULE[ModuleFuelTanks],*{}

MODULE
{
name = ModuleFuelTanks
type = HTPB
volume = 16780
basemass = -1

// HTPB/AP propellant mixture mass 29700 Kg.

TANK
{
name = HTPB
amount = 16780
maxAmount = 16780
}
}

MODULE
{
name = ModuleEngineConfigs
type = ModuleEngines
configuration = GEM-60/TVC
origMass = 3.952
origMass = 3.380
modded = false

CONFIG
{
name = GEM-60/TVC
minThrust = 1236
maxThrust = 1236
minThrust = 1235.947
maxThrust = 1235.947
heatProduction = 100
gimbalRange = 5.0

@@ -171,11 +193,11 @@
CONFIG
{
name = GEM-60/Fixed
minThrust = 1236
maxThrust = 1236
minThrust = 1248.91
maxThrust = 1248.91
gimbalRange = 0
heatProduction = 100
massMult = 0.844
massMult = 0.9822

PROPELLANT
{
@@ -291,8 +313,4 @@
}
}
}

!MODULE[ModuleAlternator],*{}

!RESOURCE,*{}
}
Original file line number Diff line number Diff line change
@@ -179,13 +179,6 @@
}
}

@MODULE[ModuleGimbal]
{
@gimbalRange = 4.0
%useGimbalResponseSpeed = True
%gimbalResponseSpeed = 16
}

!MODULE[ModuleAnimateHeat],*{}

!MODULE[FXModuleAnimateThrottle],*{}
@@ -198,27 +191,6 @@
dependOnEngineState = True
dependOnThrottle = True
}

!MODULE[ModuleFuelTanks],*{}

MODULE
{
name = ModuleFuelTanks
type = HTPB
volume = 16780
basemass = -1

// HTPB/AP propellant mixture mass 29700 Kg.

TANK
{
name = HTPB
amount = 16780
maxAmount = 16780
}
}

!RESOURCE,*{}
}

// ==================================================
Original file line number Diff line number Diff line change
@@ -149,12 +149,7 @@
@manufacturer = Hercules
%tags = ATK GEM 40
@description = The 40-inch Graphite-Epoxy Motor is an innovative solid rocket motor manufactured by Alliant Techsystems for use in Delta rockets. Cheaper and more efficient than the previous Castor 4A, the GEM motor uses a graphite-epoxy caseand HTPB propellant, giving a high propellant mass fraction and specific impulse. The motor is equipped with a vectored nozzle, fixed nozzle with a 10 degree cant can also be used. It has only been used on the Delta II EELTT with RS-27A engine. This version is ground ignited. For designation purposes, the second digit denotes the number of motors attached and the first digit should be 7, as per core designation.
!RESOURCE[SolidFuel]
{
}
!RESOURCE[MonoPropellant]
{
}
!MODULE[ModuleEngineIgnitor]
{
}
@@ -184,19 +179,6 @@
}
%engineType = GEM-40
%massOffset = -0.1 //for the decoupler mass
MODULE
{
name = ModuleFuelTanks
volume = 6647.45762712
type = HTPB
basemass = -1
TANK
{
name = HTPB
amount = 6647.45762712
maxAmount = 6647.45762712
}
}
}
//remove air-lit config
@@ -237,19 +219,6 @@
}
%engineType = GEM-40
%massOffset = -0.1 //for the decoupler mass
MODULE
{
name = ModuleFuelTanks
volume = 6647.45762712
type = HTPB
basemass = -1
TANK
{
name = HTPB
amount = 6647.45762712
maxAmount = 6647.45762712
}
}
}
//remove ground-lit config
@@ -279,12 +248,6 @@
@manufacturer = ATK
%tags = ATK GEM 46
@description = The GEM-46 is a stretched and expanded (46 inch) version of GEM-40. It features a graphite-epoxy case and HTPB propellant, giving it high efficiency and a high propellant mass fraction. It also features a gimbaled nozzle, canted 5 degrees by default. A fixed nozzle version can also be used. It has been used with EELTT and SEELTT tanks. This version is ground ignited. For designation purposes, the second digit of the designation number denotes the number of boosters. When used with Delta II EELTT and replacing GEM-40 motors, the letter H is added after the fourth digit. With SEELTT, this is not done, because GEM-46 motors are used in the baseline configuration.
!RESOURCE[SolidFuel]
{
}
!RESOURCE[MonoPropellant]
{
}
!MODULE[ModuleEngineIgnitor]
{
}
@@ -294,19 +257,6 @@
}
%engineType = GEM-46
%massOffset = -0.1 //for the decoupler mass
MODULE
{
name = ModuleFuelTanks
volume = 9528.0022
type = HTPB
basemass = -1
TANK
{
name = HTPB
amount = 9528.0022
maxAmount = 9528.0022
}
}
}
//remove air-lit config
@@ -336,30 +286,11 @@
@manufacturer = ATK
%tags = ATK GEM 46
@description = The GEM-46 is a stretched and expanded version of GEM-40. It features a graphite-epoxy case and HTPB propellant, giving it high efficiency and a high propellant mass fraction. This version has no gimbal, with the fixed nozzle cant of 5 degrees. It has been used with EELTT and SEELTT tanks. This version is air ignited and also features an extended nozzle for improved altiude performance. For designation purposes, the second digit should be 9 if air-lit motors are used (if there are less than 9 motors, all are ground lit). When used with Delta II EELTT and replacing GEM-40 motors, the letter H is added after the fourth digit. With SEELTT, this is not done, because GEM-46 motors are used in the baseline configuration.
!RESOURCE[SolidFuel]
{
}
!RESOURCE[MonoPropellant]
{
}
!MODULE[ModuleEngineIgnitor]
{
}
%engineType = GEM-46
%massOffset = -0.1 //for the decoupler mass
MODULE
{
name = ModuleFuelTanks
volume = 9528.0022
type = HTPB
basemass = -1
TANK
{
name = HTPB
amount = 9528.0022
maxAmount = 9528.0022
}
}
}
//limit to air-lit config
Original file line number Diff line number Diff line change
@@ -243,32 +243,10 @@
%breakingTorque = 250
@maxTemp = 1073.15
%tags = Delta IV GEM-60 GEM
!RESOURCE[SolidFuel]
{
}
!RESOURCE[MonoPropellant]
{
}
!MODULE[ModuleEngineIgnitor]
{
}
@MODULE[ModuleGimbal]
{
@gimbalRange = 5
}
%engineType = GEM-60
%massOffset = -0.2 //for the decoupler mass
MODULE
{
name = ModuleFuelTanks
volume = 16778.3051
type = HTPB
basemass = -1
TANK
{
name = HTPB
amount = 16778.3051
maxAmount = 16778.3051
}
}
}
Original file line number Diff line number Diff line change
@@ -213,10 +213,6 @@
gimbalTransformName = NozzleTransform
gimbalRange = 5 //2012 ATK Motor Catalog
}
@MODULE[ModuleFuelTanks]
{
@volume = 16778.24
}
%engineType = GEM-60
}
// ########################################################################################## GEM46
@@ -247,10 +243,7 @@
gimbalTransformName = NozzleTransform
gimbalRange = 5 //2012 ATK Motor Catalog
}
@MODULE[ModuleFuelTanks]
{
@volume = 9528
}
!MODULE[ModuleFuelTanks] {}
%engineType = GEM-46
}
// ########################################################################################## Globe VI SRB
@@ -644,16 +637,6 @@
{
@gimbalRange = 5.0
}
!RESOURCE[SolidFuel]
{
}
MODULE
{
name = ModuleFuelTanks
volume = 16778.2
type = HTPB
basemass = -1
}
%engineType = GEM-60
}
// ########################################################################################## Globe X SRB
@@ -694,16 +677,7 @@
{
@gimbalRange = 5.0
}
!RESOURCE[SolidFuel]
{
}
MODULE
{
name = ModuleFuelTanks
volume = 9528
type = HTPB
basemass = -1
}
%engineType = GEM-46
}
// ########################################################################################## Globe X-10S "Thor II" SRB

Large diffs are not rendered by default.

Original file line number Diff line number Diff line change
@@ -228,26 +228,7 @@
!MODULE[ModuleFuelTanks],*{}
MODULE
{
name = ModuleFuelTanks
type = HTPB
volume = 6647
basemass = -1
// HTPB/AP propellant mixture mass 11765 Kg.
TANK
{
name = HTPB
amount = 6647
maxAmount = 6647
}
}
!MODULE[ModuleGimbal],*{}
!RESOURCE,*{}
}
// ==================================================
@@ -313,26 +294,7 @@
!MODULE[ModuleFuelTanks],*{}
MODULE
{
name = ModuleFuelTanks
type = HTPB
volume = 9528
basemass = -1
// HTPB/AP propellant mixture mass 16864 Kg.
TANK
{
name = HTPB
amount = 9528
maxAmount = 9528
}
}
!MODULE[ModuleGimbal],*{}
!RESOURCE,*{}
}
// ==================================================
@@ -407,23 +369,6 @@
!MODULE[ModuleFuelTanks],*{}
MODULE
{
name = ModuleFuelTanks
type = HTPB
volume = 9528
basemass = -1
// HTPB/AP propellant mixture mass 16864 Kg.
TANK
{
name = HTPB
amount = 9528
maxAmount = 9528
}
}
!MODULE[ModuleGimbal],*{}
MODULE
@@ -434,8 +379,6 @@
useGimbalResponseSpeed = True
gimbalResponseSpeed = 16
}
!RESOURCE,*{}
}
// ==================================================
@@ -509,27 +452,6 @@
%useGimbalResponseSpeed = True
%gimbalResponseSpeed = 16
}
!MODULE[ModuleFuelTanks],*{}
MODULE
{
name = ModuleFuelTanks
type = HTPB
volume = 16780
basemass = -1
// HTPB/AP propellant mixture mass 29700 Kg.
TANK
{
name = HTPB
amount = 16780
maxAmount = 16780
}
}
!RESOURCE,*{}
}
// ==================================================

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