Difference between revisions of "Parts/Aero/airlinerWings/TailFin.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, 1.0, 0.0, 1.0, 0.0, 0.0, 1
 
node_attach = 0.0, 1.0, 0.0, 1.0, 0.0, 0.0, 1
 +
CoLOffset = 0.75, 0.25, 0
 +
CoPOffset = 0.75, 0.25, 0
 
CoMOffset = -2.0, 0.4, 0
 
CoMOffset = -2.0, 0.4, 0
 
TechRequired = experimentalAerodynamics
 
TechRequired = experimentalAerodynamics

Revision as of 12:13, 27 June 2015

This is the configuration file for FAT-455 Aeroplane Tail Fin.
PART
{
	name = airlinerTailFin
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 1.0, 0.0, 1.0, 0.0, 0.0, 1
	CoLOffset = 0.75, 0.25, 0
	CoPOffset = 0.75, 0.25, 0
	CoMOffset = -2.0, 0.4, 0
	TechRequired = experimentalAerodynamics
	entryCost = 4000
	cost = 1000
	category = Aero
	subcategory = 0
	title = FAT-455 Aeroplane Tail Fin
	manufacturer = WinterOwl Aircraft Emporium
	description = Large conventional wing with built-in control surface.
	attachRules = 0,1,0,1,1
	mass = 0.36
	thermalMassModifier = 3.0
	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/TailFin
	}
	MODULE
	{
		name = ModuleControlSurface
		useInternalDragModel = True
		dragCoeff = 0.6
		deflectionLiftCoeff = 2.69 	// area = 9.48m^2
		ctrlSurfaceRange = 15
		ctrlSurfaceArea = 0.37 	// area = 3.45m^2
		actuatorSpeed = 15
		transformName = ctrlSrf
	}
}