// wos-A6-winglet.cfg v1.1.0.0
// Wernher's Old Stuff (WOS)
// created: 
// updated: 10 Dec 2022

// this file: CC BY-SA 4.0 by zer0Kerbal

PART
{
	name = wos-A6-winglet
	// Wing4Redstone
	module = Part
	author = TD and zer0Kerbal

	MODEL
	{
		model = WernhersOldStuff/Assets/A6-winglet
	}
	scale = 1.0
	rescaleFactor = 0.703
	bulkheadProfiles = srf

	attachRules = 0,1,0,0,1
	//node_stack = -0.88, -0.745, 0.0, 1.0, 0.0, 0.0
	node_attach = -0.88, -0.745, 0.0, 1.0, 0.0, 0.0, 1, 1

	TechRequired = start
	entryCost = 4600
	cost = 600
	category = Aero
	subcategory = 0

	title = #WOS-A6-winglet-titl
	manufacturer = #WOS-Agency-titl
	description = #WOS-A6-winglet-desc
	tags = #autoLOC_500225 // aero aircraft fin lift plane rocket stab swept

	mass = 0.0196
	explosionPotential = 0.1
	
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 5
	//CoLOffset = -1.14, -0.74, 0.0
	//CoPOffset = -1.14, -0.74, 0.0
	//CoMOffset = -1.14, -1.2, 0.0

	crashTolerance = 12

	maxTemp = 2400
	thermalMassModifier = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95

	MODULE
	{
		name = ModuleControlSurface
		useInternalDragModel = True
		dragCoeff = 0.4
		deflectionLiftCoeff = 0.33   //2.69 = area = 9.48m^2
		ctrlSurfaceRange = 25
		ctrlSurfaceArea =  0.18 //0.37 	// area = 3.45m^2
		actuatorSpeed = 24
		transformName = obj_ctrlSrf
	}

	// Dimensions: x: 1.38, y: 2.27, z: 0.37
	// Bounding Box Size: 1149.323 liters
	MODULE
	{
		name = ModuleCargoPart
		packedVolume = 1250
	}

	DRAG_CUBE
	{
		cube = neutral, 0.4614,0.99,0.611, 0.4614,0.6304,1.123, 0.1659,0.3989,2.283, 0.1659,0.9272,1.616, 0.9731,0.9525,0.2829, 0.9731,0.9527,0.2829, -0.7752,-0.4695,0, 1.204,2.267,0.3681
		cube = fullDeflectionPos, 0.4794,0.99,0.9523, 0.4794,0.6686,1.123, 0.2571,0.5746,2.283, 0.2571,0.7459,1.626, 0.9487,0.9282,0.4367, 0.9487,0.9022,0.4776, -0.7752,-0.4695,0.01852, 1.204,2.267,0.4513
		cube = fullDeflectionNeg, 0.4794,0.99,0.9523, 0.4794,0.6686,1.123, 0.2571,0.5712,2.283, 0.2571,0.7433,1.626, 0.9487,0.9022,0.4776, 0.9487,0.9291,0.4367, -0.7752,-0.4695,-0.01852, 1.204,2.267,0.4513
	}
}