Difference between revisions of "Parts/Aero/airlinerWings/MainWing.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 = -2.5, 0.25, 0
 +
CoPOffset = -2.5, 0.25, 0
 
TechRequired = experimentalAerodynamics
 
TechRequired = experimentalAerodynamics
 
entryCost = 36400
 
entryCost = 36400

Revision as of 12:13, 27 June 2015

This is the configuration file for FAT-455 Aeroplane Main Wing.
PART
{
	name = airlinerMainWing
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	CoLOffset = -2.5, 0.25, 0
	CoPOffset = -2.5, 0.25, 0
	TechRequired = experimentalAerodynamics
	entryCost = 36400
	cost = 2800
	category = Aero
	subcategory = 0
	title = FAT-455 Aeroplane Main Wing
	manufacturer = WinterOwl Aircraft Emporium
	description = One of the largest lifting surfaces in production. The internal volume of these is big enough to carry generously sized fuel tanks.
	attachRules = 0,1,0,1,1
	mass = 0.78
	thermalMassModifier = 3
	heatConductivity = 0.12
	emissiveConstant = 0.4
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 2
	crashTolerance = 15
	maxTemp = 1200 // = 3400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	MODEL
	{
		model = Squad/Parts/Aero/airlinerWings/MainWing
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 7.8		// 27,41m^2
		dragAtMaxAoA = 0.6
		dragAtMinAoA = 0.0
	}
	RESOURCE
	{
		name = LiquidFuel
		amount = 0		//empty by default
		maxAmount = 600
	}
}