Difference between revisions of "Parts/Aero/shuttleWings/delta.cfg"

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(+added in 1.0;)
 
m (*update to 1.0.4;)
 
Line 6: Line 6:
 
rescaleFactor = 1
 
rescaleFactor = 1
 
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
 
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
 +
CoLOffset = -1.6, -0.4, 0
 +
CoPOffset = -1.6, -0.4, 0
 
TechRequired = aerospaceTech
 
TechRequired = aerospaceTech
 
entryCost = 36400
 
entryCost = 36400
Line 16: Line 18:
 
attachRules = 0,1,0,1,1
 
attachRules = 0,1,0,1,1
 
mass = 0.5
 
mass = 0.5
thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K
+
thermalMassModifier = 8.0
 
heatConductivity = 0.06 // half default
 
heatConductivity = 0.06 // half default
 
emissiveConstant = 0.95
 
emissiveConstant = 0.95
Line 24: Line 26:
 
angularDrag = 2
 
angularDrag = 2
 
crashTolerance = 15
 
crashTolerance = 15
maxTemp = 2000 // = 3400
+
maxTemp = 2400
 
explosionPotential = 0.1
 
explosionPotential = 0.1
 
fuelCrossFeed = True
 
fuelCrossFeed = True

Latest revision as of 12:10, 27 June 2015

This is the configuration file for Big-S Delta Wing.
PART
{
	name = wingShuttleDelta
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	CoLOffset = -1.6, -0.4, 0
	CoPOffset = -1.6, -0.4, 0
	TechRequired = aerospaceTech
	entryCost = 36400
	cost = 3000
	category = Aero
	subcategory = 0
	title = Big-S Delta Wing
	manufacturer = C7 Aerospace Division
	description = The Big-S line of wings are C7's largest lifting surfaces to date. Not only are they Sturdy and heat resistant enough to survive reentry, but also have enough internal volume to carry optional fuel tanks.
	attachRules = 0,1,0,1,1
	mass = 0.5
	thermalMassModifier = 8.0
	heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 2
	crashTolerance = 15
	maxTemp = 2400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	MODEL
	{
		model = Squad/Parts/Aero/shuttleWings/ShuttleDeltaWing
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 5.0		// 16,5m^2
		dragAtMaxAoA = 0.6
		dragAtMinAoA = 0.0
	}
	RESOURCE
	{
		name = LiquidFuel
		amount = 0		//unusual for shuttle wings, empty by default
		maxAmount = 300
	}
}