Difference between revisions of "Parts/Engine/liquidEngineMk55/liquidEngineMk55.cfg"

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m (*update to 0.90.0;)
m (*update to 1.0;)
Line 1: Line 1:
{{Part config|Rockomax Mark 55 Radial Mount Liquid Engine|2=PART
+
{{Part config|Mk-55 "Thud" Liquid Fuel Engine|2=PART
 
{
 
{
// Kerbal Space Program - Part Config
+
name = radialLiquidEngine1-2
// Mk-55 Liquid Fuel Engine
+
module = Part
//
+
author = NovaSilisko
 
+
mesh = model.mu
// --- general parameters ---
+
rescaleFactor = 1
name = radialLiquidEngine1-2
+
node_attach = 0.0, 0.3423436, -0.5857153, 0.0, 0.0, 1.0
module = Part
+
fx_exhaustFlame_blue_small = 0.0, -0.5337813, 0.1355984, 0.0, 1.0, 0.0, running
author = NovaSilisko
+
fx_exhaustLight_blue = 0.0, -0.5337813, 0.1355984, 0.0, 0.0, 1.0, running
 
+
sound_vent_medium = engage
// --- asset parameters ---
+
sound_rocket_hard = running
mesh = model.mu
+
sound_vent_soft = disengage
 
+
sound_explosion_low = flameout
rescaleFactor = 1
+
TechRequired = advRocketry
 
+
entryCost = 3500
// --- node definitions ---
+
cost = 820
node_attach = 0.0, 0.3423436, -0.5857153, 0.0, 0.0, 1.0
+
category = Engine
 
+
subcategory = 0
 
+
title = Mk-55 "Thud" Liquid Fuel Engine
// --- FX definitions ---
+
manufacturer = Rockomax Conglomerate
 
+
description = After an intensive search for an engineer crazy enough to plan and build a revolutionary new engine type, researchers turned to  renowned engineer Eumon Kerman, one of the top minds in the industry. He failed miserably at the job, and this is what we ended up with.
fx_exhaustFlame_blue_small = 0.0, -0.5337813, 0.1355984, 0.0, 1.0, 0.0, running
+
attachRules = 0,1,0,1,0
fx_exhaustLight_blue = 0.0, -0.5337813, 0.1355984, 0.0, 0.0, 1.0, running
+
mass = 0.9
 
+
// heatConductivity = 0.06 // half default
// --- Sound FX definition ---
+
emissiveConstant = 0.8 // engine nozzles are good at radiating.
 
+
dragModelType = default
sound_vent_medium = engage
+
maximum_drag = 0.2
sound_rocket_hard = running
+
minimum_drag = 0.2
sound_vent_soft = disengage
+
angularDrag = 2
sound_explosion_low = flameout
+
crashTolerance = 7
 
+
breakingForce = 200
// --- editor parameters ---
+
breakingTorque = 200
TechRequired = advRocketry
+
maxTemp = 2000 // = 3600
entryCost = 3500
+
bulkheadProfiles = srf
cost = 800
+
MODULE
category = Engine
+
{
subcategory = 0
+
name = ModuleEngines
title = Rockomax Mark 55 Radial Mount Liquid Engine
+
thrustVectorTransformName = thrustTransform
manufacturer = Rockomax Conglomerate
+
exhaustDamage = True
description = After an intensive search for an engineer crazy enough to plan and build a revolutionary new engine type, researchers turned to  renowned engineer Eumon Kerman, one of the top minds in the industry. He failed miserably at the job, and this is what we ended up with.
+
ignitionThreshold = 0.1
 
+
minThrust = 0
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
maxThrust = 108.1967213
attachRules = 0,1,0,1,0
+
heatProduction = 160
 
+
fxOffset = 0, 0, 0.1
// --- standard part parameters ---
+
EngineType = LiquidFuel
mass = 0.9
+
PROPELLANT
dragModelType = default
+
{
maximum_drag = 0.2
+
name = LiquidFuel
minimum_drag = 0.2
+
ratio = 0.9
angularDrag = 2
+
DrawGauge = True
crashTolerance = 7
+
}
breakingForce = 200
+
PROPELLANT
breakingTorque = 200
+
{
maxTemp = 3600
+
name = Oxidizer
 
+
ratio = 1.1
// --- liquid engine parameters ---
+
}
 
+
atmosphereCurve
MODULE
+
{
{
+
key = 0 305
name = ModuleEngines
+
key = 1 275
thrustVectorTransformName = thrustTransform
+
key = 9 0.001
exhaustDamage = True
+
}
ignitionThreshold = 0.1
+
}
minThrust = 0
+
MODULE
maxThrust = 120
+
{
heatProduction = 350
+
name = ModuleGimbal
fxOffset = 0, 0, 0.1
+
gimbalTransformName = thrustTransform
PROPELLANT
+
gimbalRange = 8
 +
}
 +
MODULE
 
{
 
{
name = LiquidFuel
+
name = ModuleTestSubject
ratio = 0.9
+
environments = 15
DrawGauge = True
+
useStaging = True
 +
useEvent = True
 
}
 
}
PROPELLANT
+
MODULE
 
{
 
{
name = Oxidizer
+
name = ModuleSurfaceFX
ratio = 1.1
+
thrustProviderModuleIndex = 0
 +
fxMax = 0.5
 +
maxDistance = 30
 +
falloff = 1.7
 +
thrustTransformName = thrustTransform
 
}
 
}
atmosphereCurve
 
{
 
key = 0 360
 
key = 1 320
 
}
 
 
}
 
 
MODULE
 
{
 
name = ModuleGimbal
 
gimbalTransformName = thrustTransform
 
gimbalRange = 5
 
}
 
 
MODULE
 
{
 
name = ModuleTestSubject
 
 
// nowhere: 0, srf: 1, ocean: 2, atmo: 4, space: 8
 
environments = 15
 
 
useStaging = True
 
useEvent = True
 
}
 
 
}
 
}
  
 
}}
 
}}

Revision as of 17:53, 29 April 2015

This is the configuration file for Mk-55 "Thud" Liquid Fuel Engine.
PART
{
	name = radialLiquidEngine1-2
	module = Part
	author = NovaSilisko
	mesh = model.mu
	rescaleFactor = 1
	node_attach = 0.0, 0.3423436, -0.5857153, 0.0, 0.0, 1.0
	fx_exhaustFlame_blue_small = 0.0, -0.5337813, 0.1355984, 0.0, 1.0, 0.0, running
	fx_exhaustLight_blue = 0.0, -0.5337813, 0.1355984, 0.0, 0.0, 1.0, running
	sound_vent_medium = engage
	sound_rocket_hard = running
	sound_vent_soft = disengage
	sound_explosion_low = flameout
	TechRequired = advRocketry
	entryCost = 3500
	cost = 820
	category = Engine
	subcategory = 0
	title = Mk-55 "Thud" Liquid Fuel Engine
	manufacturer = Rockomax Conglomerate
	description = After an intensive search for an engineer crazy enough to plan and build a revolutionary new engine type, researchers turned to  renowned engineer Eumon Kerman, one of the top minds in the industry. He failed miserably at the job, and this is what we ended up with.
	attachRules = 0,1,0,1,0
	mass = 0.9
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.8 // engine nozzles are good at radiating.
	dragModelType = default
	maximum_drag = 0.2
	minimum_drag = 0.2
	angularDrag = 2
	crashTolerance = 7
	breakingForce = 200
	breakingTorque = 200
	maxTemp = 2000 // = 3600
	bulkheadProfiles = srf
	MODULE
	{
		name = ModuleEngines
		thrustVectorTransformName = thrustTransform
		exhaustDamage = True
		ignitionThreshold = 0.1
		minThrust = 0
		maxThrust = 108.1967213
		heatProduction = 160
		fxOffset = 0, 0, 0.1
		EngineType = LiquidFuel
		PROPELLANT
		{
			name = LiquidFuel
			ratio = 0.9
			DrawGauge = True
		}
		PROPELLANT
		{
			name = Oxidizer
			ratio = 1.1
		}
		atmosphereCurve
		{
			key = 0 305
			key = 1 275
			key = 9 0.001
		}
	}
	MODULE
	{
		name = ModuleGimbal
		gimbalTransformName = thrustTransform
		gimbalRange = 8
	}
	MODULE
	{
		name = ModuleTestSubject
		environments = 15
		useStaging = True
		useEvent = True
	}
	MODULE
	{
		name = ModuleSurfaceFX
		thrustProviderModuleIndex = 0
		fxMax = 0.5
		maxDistance = 30
		falloff = 1.7
		thrustTransformName = thrustTransform
	}
}