Difference between revisions of "Parts/Aero/wings/structural4.cfg"

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(+added in 0.25;)
 
m (Update config)
 
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{{Part config|Structural Wing Type D|2=PART
 
{{Part config|Structural Wing Type D|2=PART
 
{
 
{
 
+
name = structuralWing4
name = structuralWing4
+
module = Part
module = Part
+
author = Porkjet
author = Porkjet
+
rescaleFactor = 1
 
+
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
MODEL
+
CoMOffset = -0.236, -0.1, 0
{
+
CoLOffset = -0.236, -0.1, 0
model = Squad/SPP/Wings/structural4
+
CoPOffset = -0.236, -0.1, 0
 +
TechRequired = advAerodynamics
 +
entryCost = 6400
 +
cost = 150
 +
category = Aero
 +
subcategory = 0
 +
title = #autoLOC_500277 //#autoLOC_500277 = Structural Wing Type D
 +
manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
 +
description = #autoLOC_500278 //#autoLOC_500278 = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish.
 +
attachRules = 0,1,0,1,1
 +
mass = 0.025
 +
thermalMassModifier = 8.0
 +
// heatConductivity = 0.06 // half default
 +
emissiveConstant = 0.95
 +
dragModelType = none
 +
maximum_drag = 0.02
 +
minimum_drag = 0.02
 +
angularDrag = 1
 +
crashTolerance = 15
 +
maxTemp = 2400
 +
explosionPotential = 0.1
 +
fuelCrossFeed = True
 +
bulkheadProfiles = srf
 +
tags = #autoLOC_500279 //#autoLOC_500279 = aero aircraft fligh foil lift plane swept
 +
MODEL
 +
{
 +
model = Squad/Parts/Aero/wings/structural4
 +
}
 +
MODULE
 +
{
 +
name = ModuleLiftingSurface
 +
useInternalDragModel = True
 +
deflectionLiftCoeff = 0.25
 +
dragAtMaxAoA = 0.08
 +
dragAtMinAoA = 0.0
 +
}
 +
MODULE
 +
{
 +
name = ModuleCargoPart
 +
packedVolume = 450
 +
}
 
}
 
}
 
 
rescaleFactor = 1
 
 
 
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
 
 
// --- editor parameters ---
 
TechRequired = advAerodynamics
 
entryCost = 6400
 
cost = 150
 
category = Aero
 
subcategory = 0
 
title = Structural Wing Type D
 
manufacturer = C7 Aerospace Division
 
description = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish.
 
 
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
 
attachRules = 0,1,0,1,1
 
 
 
// --- standard part parameters ---
 
mass = 0.012
 
dragModelType = override
 
maximum_drag = 0.02
 
minimum_drag = 0.02
 
angularDrag = 1
 
crashTolerance = 15
 
maxTemp = 3400
 
explosionPotential = 0.1
 
fuelCrossFeed = True
 
 
MODULE
 
{
 
name = ModuleLiftingSurface
 
 
deflectionLiftCoeff = 0.25
 
dragAtMaxAoA = 0.08
 
dragAtMinAoA = 0.0
 
}
 
 
 
 
}
 
 
 
}}
 
}}

Latest revision as of 11:02, 13 October 2024

This is the configuration file for Structural Wing Type D.
PART
{
	name = structuralWing4
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	CoMOffset = -0.236, -0.1, 0
	CoLOffset = -0.236, -0.1, 0
	CoPOffset = -0.236, -0.1, 0
	TechRequired = advAerodynamics
	entryCost = 6400
	cost = 150
	category = Aero
	subcategory = 0
	title = #autoLOC_500277 //#autoLOC_500277 = Structural Wing Type D
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500278 //#autoLOC_500278 = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish.
	attachRules = 0,1,0,1,1
	mass = 0.025
	thermalMassModifier = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 1
	crashTolerance = 15
	maxTemp = 2400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	tags = #autoLOC_500279 //#autoLOC_500279 = aero aircraft fligh foil lift plane swept
	MODEL
	{
		model = Squad/Parts/Aero/wings/structural4
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 0.25
		dragAtMaxAoA = 0.08
		dragAtMinAoA = 0.0
	}
	MODULE
	{
		name = ModuleCargoPart
		packedVolume = 450
	}
}