Difference between revisions of "Parts/Aero/wings/structural1.cfg"

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m (BobBot moved page Parts/SPP/Wings/structural1.cfg to Parts/Aero/wings/structural1.cfg without leaving a redirect: Renamed part configuration file after update.)
m (*update to 1.0;)
Line 1: Line 1:
 
{{Part config|Structural Wing Type A|2=PART
 
{{Part config|Structural Wing Type A|2=PART
 
{
 
{
 
+
name = structuralWing
name = structuralWing
+
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
+
TechRequired = aerodynamicSystems
{
+
entryCost = 6400
model = Squad/SPP/Wings/structural1
+
cost = 500
}
+
category = Aero
 
+
subcategory = 0
 
+
title = Structural Wing Type A
rescaleFactor = 1
+
manufacturer = C7 Aerospace Division
 
+
description = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings.
 
+
attachRules = 0,1,0,1,1
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
+
mass = 0.05
 
+
thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K
// --- editor parameters ---
+
// heatConductivity = 0.06 // half default
TechRequired = aerodynamicSystems
+
emissiveConstant = 0.95
entryCost = 6400
+
dragModelType = none
cost = 500
+
maximum_drag = 0.02
category = Aero
+
minimum_drag = 0.02
subcategory = 0
+
angularDrag = 2
title = Structural Wing Type A
+
crashTolerance = 15
manufacturer = C7 Aerospace Division
+
maxTemp = 2000 // = 3400
description = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings.
+
explosionPotential = 0.1
 
+
fuelCrossFeed = True
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
bulkheadProfiles = srf
attachRules = 0,1,0,1,1
+
MODEL
 
+
{
 
+
model = Squad/Parts/Aero/wings/structural1
// --- standard part parameters ---
+
}
mass = 0.05
+
MODULE
dragModelType = override
+
{
maximum_drag = 0.02
+
name = ModuleLiftingSurface
minimum_drag = 0.02
+
useInternalDragModel = True
angularDrag = 2
+
deflectionLiftCoeff = 1
crashTolerance = 15
+
dragAtMaxAoA = 0.3
maxTemp = 3400
+
dragAtMinAoA = 0.0
explosionPotential = 0.1
+
}
fuelCrossFeed = True
 
 
 
MODULE
 
{
 
name = ModuleLiftingSurface
 
 
deflectionLiftCoeff = 1
 
dragAtMaxAoA = 0.3
 
dragAtMinAoA = 0.0
 
}
 
 
 
 
}
 
}
  
 
}}
 
}}

Revision as of 10:40, 29 April 2015

This is the configuration file for Structural Wing Type A.
PART
{
	name = structuralWing
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	TechRequired = aerodynamicSystems
	entryCost = 6400
	cost = 500
	category = Aero
	subcategory = 0
	title = Structural Wing Type A
	manufacturer = C7 Aerospace Division
	description = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings.
	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/structural1
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 1
		dragAtMaxAoA = 0.3
		dragAtMinAoA = 0.0
	}
}