Difference between revisions of "Parts/Engine/liquidEngineLV-1/liquidEngineLV-1.cfg"

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<pre>
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{{Part config|LV-1 "Ant" Liquid Fuel Engine|2=PART
name = microEngine
 
module = Part
 
author = NovaSilisko
 
 
 
mesh = model.mu
 
scale = 1
 
rescaleFactor = 1
 
 
 
node_stack_top = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0
 
node_stack_bottom = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, 0
 
 
 
fx_exhaustFlame_white_tiny = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, running
 
 
 
sound_vent_medium = engage
 
sound_rocket_mini = running
 
sound_vent_soft = disengage
 
sound_explosion_low = flameout
 
 
 
cost = 150
 
category = Propulsion
 
subcategory = 0
 
title = LV-1 Liquid Fuel Engine
 
manufacturer = Jebediah Kerman's Junkyard and Spaceship Parts Co.
 
description = What is this, an engine for ants?
 
attachRules = 1,0,1,0,0
 
 
 
mass = 0.03
 
dragModelType = default
 
maximum_drag = 0.2
 
minimum_drag = 0.2
 
angularDrag = 2
 
crashTolerance = 7
 
maxTemp = 3600
 
 
 
MODULE
 
 
{
 
{
name = ModuleEngines
+
name = microEngine
thrustVectorTransformName = thrustTransform
+
module = Part
exhaustDamage = False
+
author = NovaSilisko
ignitionThreshold = 0.1
+
mesh = model.mu
minThrust = 0
+
scale = 1
maxThrust = 1.5
+
rescaleFactor = 1
heatProduction = 30
+
node_stack_top = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0
fxOffset = 0, 0, 0.02
+
node_stack_bottom = 0.0, -0.2816985, 0.0, 0.0, -1.0, 0.0, 0
PROPELLANT
+
fx_exhaustFlame_white_tiny = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, running
 +
sound_vent_medium = engage
 +
sound_rocket_mini = running
 +
sound_vent_soft = disengage
 +
sound_explosion_low = flameout
 +
TechRequired = propulsionSystems
 +
entryCost = 1500
 +
cost = 110
 +
category = Engine
 +
subcategory = 0
 +
title = LV-1 "Ant" Liquid Fuel Engine
 +
manufacturer = Jebediah Kerman's Junkyard and Spacecraft Parts Co
 +
description = What is this, an engine for ants?
 +
attachRules = 1,0,1,0,0
 +
mass = 0.02
 +
// heatConductivity = 0.06 // half default
 +
skinInternalConductionMult = 4.0
 +
emissiveConstant = 0.8 // engine nozzles are good at radiating.
 +
dragModelType = default
 +
maximum_drag = 0.2
 +
minimum_drag = 0.2
 +
angularDrag = 2
 +
crashTolerance = 7
 +
maxTemp = 2000 // = 3600
 +
bulkheadProfiles = size0
 +
MODULE
 
{
 
{
name = LiquidFuel
+
name = ModuleEngines
        ratio = 0.9
+
thrustVectorTransformName = thrustTransform
 +
exhaustDamage = False
 +
ignitionThreshold = 0.1
 +
minThrust = 0
 +
maxThrust = 2
 +
heatProduction = 25
 +
fxOffset = 0, 0, 0.02
 +
EngineType = LiquidFuel
 +
PROPELLANT
 +
{
 +
name = LiquidFuel
 +
ratio = 0.9
 +
DrawGauge = True
 +
}
 +
PROPELLANT
 +
{
 +
name = Oxidizer
 +
ratio = 1.1
 +
}
 +
atmosphereCurve
 +
{
 +
key = 0 315
 +
key = 1 80
 +
key = 3 0.001
 +
}
 
}
 
}
PROPELLANT
+
MODULE
 
{
 
{
name = Oxidizer
+
name = ModuleTestSubject
ratio = 1.1
+
environments = 8
 +
useStaging = False
 +
useEvent = True
 
}
 
}
atmosphereCurve
 
{
 
  key = 0 290
 
  key = 1 220
 
}
 
 
 
}
 
}
</pre>
+
 
 +
}}

Latest revision as of 12:24, 27 June 2015

This is the configuration file for LV-1 "Ant" Liquid Fuel Engine.
PART
{
	name = microEngine
	module = Part
	author = NovaSilisko
	mesh = model.mu
	scale = 1
	rescaleFactor = 1
	node_stack_top = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0
	node_stack_bottom = 0.0, -0.2816985, 0.0, 0.0, -1.0, 0.0, 0
	fx_exhaustFlame_white_tiny = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, running
	sound_vent_medium = engage
	sound_rocket_mini = running
	sound_vent_soft = disengage
	sound_explosion_low = flameout
	TechRequired = propulsionSystems
	entryCost = 1500
	cost = 110
	category = Engine
	subcategory = 0
	title = LV-1 "Ant" Liquid Fuel Engine
	manufacturer = Jebediah Kerman's Junkyard and Spacecraft Parts Co
	description = What is this, an engine for ants?
	attachRules = 1,0,1,0,0
	mass = 0.02
	// heatConductivity = 0.06 // half default
	skinInternalConductionMult = 4.0
	emissiveConstant = 0.8 // engine nozzles are good at radiating.
	dragModelType = default
	maximum_drag = 0.2
	minimum_drag = 0.2
	angularDrag = 2
	crashTolerance = 7
	maxTemp = 2000 // = 3600
	bulkheadProfiles = size0
	MODULE
	{
		name = ModuleEngines
		thrustVectorTransformName = thrustTransform
		exhaustDamage = False
		ignitionThreshold = 0.1
		minThrust = 0
		maxThrust = 2
		heatProduction = 25
		fxOffset = 0, 0, 0.02
		EngineType = LiquidFuel
		PROPELLANT
		{
			name = LiquidFuel
			ratio = 0.9
			DrawGauge = True
		}
		PROPELLANT
		{
			name = Oxidizer
			ratio = 1.1
		}
		atmosphereCurve
		{
			key = 0 315
			key = 1 80
			key = 3 0.001
		}
	}
	MODULE
	{
		name = ModuleTestSubject
		environments = 8
		useStaging = False
		useEvent = True
	}
}