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

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m (*update to 1.0;)
m (*update to 1.0.1;)
Line 15: Line 15:
 
sound_explosion_low = flameout
 
sound_explosion_low = flameout
 
TechRequired = propulsionSystems
 
TechRequired = propulsionSystems
entryCost = 4000
+
entryCost = 1500
 
cost = 110
 
cost = 110
 
category = Engine
 
category = Engine
Line 40: Line 40:
 
ignitionThreshold = 0.1
 
ignitionThreshold = 0.1
 
minThrust = 0
 
minThrust = 0
maxThrust = 0.54
+
maxThrust = 2
heatProduction = 8.095
+
heatProduction = 25
 
fxOffset = 0, 0, 0.02
 
fxOffset = 0, 0, 0.02
 
EngineType = LiquidFuel
 
EngineType = LiquidFuel

Revision as of 20:49, 1 May 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
	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 85
			key = 3 0.001
		}
	}
	MODULE
	{
		name = ModuleTestSubject
		environments = 8
		useStaging = False
		useEvent = True
	}
}