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 1.0.4;)
 
(2 intermediate revisions by the same user not shown)
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 = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1
MODEL
+
CoLOffset = -0.7, -0.6, 0
{
+
CoPOffset = -0.7, -0.6, 0
model = Squad/SPP/Wings/structural1
+
TechRequired = aerodynamicSystems
}
+
entryCost = 6400
 
+
cost = 500
 
+
category = Aero
rescaleFactor = 1
+
subcategory = 0
 
+
title = Structural Wing Type A
 
+
manufacturer = C7 Aerospace Division
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
+
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
// --- editor parameters ---
+
mass = 0.1
TechRequired = aerodynamicSystems
+
thermalMassModifier = 8.0 // the dang things are light, so 3200 kJ/tonne-K
entryCost = 6400
+
// heatConductivity = 0.06 // half default
cost = 500
+
emissiveConstant = 0.95
category = Aero
+
dragModelType = none
subcategory = 0
+
maximum_drag = 0.02
title = Structural Wing Type A
+
minimum_drag = 0.02
manufacturer = C7 Aerospace Division
+
angularDrag = 2
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.
+
crashTolerance = 15
 
+
maxTemp = 2400 // = 3400
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
explosionPotential = 0.1
attachRules = 0,1,0,1,1
+
fuelCrossFeed = True
 
+
bulkheadProfiles = srf
 
+
MODEL
// --- standard part parameters ---
+
{
mass = 0.05
+
model = Squad/Parts/Aero/wings/structural1
dragModelType = override
+
}
maximum_drag = 0.02
+
MODULE
minimum_drag = 0.02
+
{
angularDrag = 2
+
name = ModuleLiftingSurface
crashTolerance = 15
+
useInternalDragModel = True
maxTemp = 3400
+
deflectionLiftCoeff = 1
explosionPotential = 0.1
+
dragAtMaxAoA = 0.3
fuelCrossFeed = True
+
dragAtMinAoA = 0.0
 
+
}
MODULE
 
{
 
name = ModuleLiftingSurface
 
 
deflectionLiftCoeff = 1
 
dragAtMaxAoA = 0.3
 
dragAtMinAoA = 0.0
 
}
 
 
 
 
}
 
}
  
 
}}
 
}}

Latest revision as of 12:10, 27 June 2015

This is the configuration file for Structural Wing Type A.
PART
{
	name = structuralWing
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	CoLOffset = -0.7, -0.6, 0
	CoPOffset = -0.7, -0.6, 0
	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 = 0.1
	thermalMassModifier = 8.0 // 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 = 2400 // = 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
	}
}