Parts/Aero/airplaneFins/tailfin.cfg

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This is the configuration file for Tail Fin.
PART
{
	name = tailfin
	module = Part
	author = C. Jenkins, Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0, 1
	CoMOffset = 0.75, -0.5, 0
	CoLOffset = 0.75, -0.5, 0
	CoPOffset = 0.75, -0.5, 0
	TechRequired = aviation
	entryCost = 3800
	cost = 600
	category = Aero
	subcategory = 0
	title = #autoLOC_500136 //#autoLOC_500136 = Tail Fin
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500137 //#autoLOC_500137 = This tailfin has passed extensive modeling in our patented P.A.S system.(Paper Airplane Simulation). This fin has been blunted to prevent accidental dismemberment of installing technicians.
	attachRules = 0,1,0,1,0
	mass = 0.125
	thermalMassModifier = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 2
	crashTolerance = 12
	maxTemp = 2400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	tags = #autoLOC_500138 //#autoLOC_500138 = aero (air canard control (elev fligh (fore lift plane )rudder stab swept
	MODEL
	{
		model = Squad/Parts/Aero/airplaneFins/TailFin
	}
	MODULE
	{
		name = ModuleControlSurface
		useInternalDragModel = True
		dragCoeff = 0.6
		deflectionLiftCoeff = 0.61		// 2.18m^2
		ctrlSurfaceRange = 25
		ctrlSurfaceArea = 1
		actuatorSpeed = 25
		transformName = ctrlSrf
	}
	MODULE
	{
		name = ModuleCargoPart		
		packedVolume = -1
	}
}