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

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m (*update to 1.0;)
m (Update config)
 
(2 intermediate revisions by one other user not shown)
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
TechRequired = highAltitudeFlight
+
CoMOffset = -0.6, 0.15, 0
 +
CoLOffset = -0.6, 0.15, 0
 +
CoPOffset = -0.6, 0.15, 0
 +
TechRequired = advAerodynamics
 
entryCost = 3200
 
entryCost = 3200
 
cost = 200
 
cost = 200
 
category = Aero
 
category = Aero
 
subcategory = 0
 
subcategory = 0
title = Small Delta Wing
+
title = #autoLOC_500247 //#autoLOC_500247 = Small Delta Wing
manufacturer = C7 Aerospace Division
+
manufacturer = #autoLOC_501624 //#autoLOC_501624 = 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.
+
description = #autoLOC_500248 //#autoLOC_500248 = 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 = 8.0
 
// heatConductivity = 0.06 // half default
 
// heatConductivity = 0.06 // half default
 
emissiveConstant = 0.95
 
emissiveConstant = 0.95
Line 24: Line 27:
 
angularDrag = 2
 
angularDrag = 2
 
crashTolerance = 15
 
crashTolerance = 15
maxTemp = 2000 // = 3400
+
maxTemp = 2400
 
explosionPotential = 0.1
 
explosionPotential = 0.1
 
fuelCrossFeed = True
 
fuelCrossFeed = True
 
bulkheadProfiles = srf
 
bulkheadProfiles = srf
 +
tags = #autoLOC_500249 //#autoLOC_500249 = aero aircraft fligh foil lift plane swept
 
MODEL
 
MODEL
 
{
 
{
Line 39: Line 43:
 
dragAtMaxAoA = 0.1
 
dragAtMaxAoA = 0.1
 
dragAtMinAoA = 0.0
 
dragAtMinAoA = 0.0
 +
}
 +
MODULE
 +
{
 +
name = ModuleCargoPart
 +
stackableQuantity = 1
 +
packedVolume = -1
 
}
 
}
 
}
 
}
 
 
}}
 
}}

Latest revision as of 11:00, 13 October 2024

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
	CoMOffset = -0.6, 0.15, 0
	CoLOffset = -0.6, 0.15, 0
	CoPOffset = -0.6, 0.15, 0
	TechRequired = advAerodynamics
	entryCost = 3200
	cost = 200
	category = Aero
	subcategory = 0
	title = #autoLOC_500247 //#autoLOC_500247 = Small Delta Wing
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500248 //#autoLOC_500248 = 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 = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 2
	crashTolerance = 15
	maxTemp = 2400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	tags = #autoLOC_500249 //#autoLOC_500249 = aero aircraft fligh foil lift plane swept
	MODEL
	{
		model = Squad/Parts/Aero/wings/delta_small
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 0.5
		dragAtMaxAoA = 0.1
		dragAtMinAoA = 0.0
	}	
	MODULE
	{
		name = ModuleCargoPart	
		stackableQuantity = 1
		packedVolume = -1
	}
}