Difference between revisions of "Parts/Aero/wings/delta small.cfg"

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m (*update to 1.0;)
m (*update to 1.0.1;)
Line 15: Line 15:
 
description = This small delta wing has breezed through extensive stress tests and design revisions, mostly because it wasn't involved in any of those. In any case, it should work as a comparatively reliable lifting surface.
 
description = This small delta wing has breezed through extensive stress tests and design revisions, mostly because it wasn't involved in any of those. In any case, it should work as a comparatively reliable lifting surface.
 
attachRules = 0,1,0,1,1
 
attachRules = 0,1,0,1,1
mass = 0.025
+
mass = 0.05
 
thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K
 
thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K
 
// heatConductivity = 0.06 // half default
 
// heatConductivity = 0.06 // half default

Revision as of 20:45, 1 May 2015

This is the configuration file for Small Delta Wing.
PART
{
	name = delta_small
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	TechRequired = highAltitudeFlight
	entryCost = 3200
	cost = 200
	category = Aero
	subcategory = 0
	title = Small Delta Wing
	manufacturer = C7 Aerospace Division
	description = This small delta wing has breezed through extensive stress tests and design revisions, mostly because it wasn't involved in any of those. In any case, it should work as a comparatively reliable lifting surface.
	attachRules = 0,1,0,1,1
	mass = 0.05
	thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 2
	crashTolerance = 15
	maxTemp = 2000 // = 3400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	MODEL
	{
		model = Squad/Parts/Aero/wings/delta_small
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 0.5
		dragAtMaxAoA = 0.1
		dragAtMinAoA = 0.0
	}
}