Difference between revisions of "Parts/Aero/wings/structural2.cfg"

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m (*update to 1.0.1;)
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 = -1.1, -0.1, 0
 +
CoPOffset = -1.1, -0.1, 0
 
TechRequired = aerodynamicSystems
 
TechRequired = aerodynamicSystems
 
entryCost = 6400
 
entryCost = 6400
Line 16: Line 18:
 
attachRules = 0,1,0,1,1
 
attachRules = 0,1,0,1,1
 
mass = 0.1
 
mass = 0.1
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 // = 3400
 
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 Structural Wing Type B.
PART
{
	name = structuralWing2
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	CoLOffset = -1.1, -0.1, 0
	CoPOffset = -1.1, -0.1, 0
	TechRequired = aerodynamicSystems
	entryCost = 6400
	cost = 500
	category = Aero
	subcategory = 0
	title = Structural Wing Type B
	manufacturer = C7 Aerospace Division
	description = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish.
	attachRules = 0,1,0,1,1
	mass = 0.1
	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 // = 3400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	MODEL
	{
		model = Squad/Parts/Aero/wings/structural2
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 1
		dragAtMaxAoA = 0.3
		dragAtMinAoA = 0.0
	}
}