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

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m (BobBot moved page Parts/Aero/structuralWing/part.cfg to Parts/Structural/structuralWing/part.cfg without leaving a redirect: Renamed part configuration file after update.)
m (Update config)
 
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{{Part config|Structural Wing|2=PART
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{{Part config|Structural Wing Type A|2=PART
 
{
 
{
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// this is a sample config file, for determining a good file format for defining part parameters
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name = structuralWing
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// comment line - ignored by cfg parser
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module = Part
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// empty lines, or lines without a '=' sign are also ignored
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author = Porkjet
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// all other lines are split at the '=' sign, and the left operand is used to know what parameter we are setting
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rescaleFactor = 1
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// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
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node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1
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// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
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CoMOffset = -0.7, -0.6, 0
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// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
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CoLOffset = -0.7, -0.6, 0
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// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
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CoPOffset = -0.7, -0.6, 0
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// This is done automatically, so any public variable defined in the loaded module can be accessed this way (provided it's value can be parsed)
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TechRequired = supersonicFlight
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entryCost = 6400
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cost = 500
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// --- general parameters ---
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category = Aero
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name = structuralWing
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subcategory = 0
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module = Winglet
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title = #autoLOC_500268 //#autoLOC_500268 = Structural Wing Type A
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author = C. Jenkins
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manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
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description = #autoLOC_500269 //#autoLOC_500269 = 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.
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// --- asset parameters ---
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attachRules = 0,1,0,1,1
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mesh = model.mu
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mass = 0.1
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scale = 0.1
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thermalMassModifier = 8.0 // the dang things are light, so 3200 kJ/tonne-K
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// heatConductivity = 0.06 // half default
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// --- editor parameters ---
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emissiveConstant = 0.95
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TechRequired = advAerodynamics
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dragModelType = none
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entryCost = 6600
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maximum_drag = 0.02
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cost = 500
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minimum_drag = 0.02
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category = Aero
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angularDrag = 2
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subcategory = 0
+
crashTolerance = 15
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title = Structural Wing
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maxTemp = 2400 // = 3400
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manufacturer = C7 Aerospace division
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explosionPotential = 0.1
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description = This wing has been constructed of surplus wing components. Comes complete with "like new" finish. Intended uses include, very large canards, and leading edges of larger delta wings.
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fuelCrossFeed = True
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bulkheadProfiles = srf
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// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
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tags = #autoLOC_500270 //#autoLOC_500270 = aero aircraft fligh foil lift plane swept
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attachRules = 0,1,0,1,1
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MODEL
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{
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// --- node definitions ---
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model = Squad/Parts/Aero/wings/structural1
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// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
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}
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node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0
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MODULE
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{
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name = ModuleLiftingSurface
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// --- standard part parameters ---
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useInternalDragModel = True
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mass = 0.05
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deflectionLiftCoeff = 1
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dragModelType = override
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dragAtMaxAoA = 0.3
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maximum_drag = 0.02
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dragAtMinAoA = 0.0
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minimum_drag = 0.02
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}
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angularDrag = 2
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MODULE
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crashTolerance = 15
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{
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maxTemp = 3400
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name = ModuleCargoPart
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explosionPotential = 0.1
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packedVolume = -1
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fuelCrossFeed = True
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}
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breakingTorque = 100
 
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// --- winglet parameters ---
 
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// dragCoeff will override the maximum_drag value
 
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dragCoeff = 0.4
 
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deflectionLiftCoeff = 1.0
 
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// --- tweakables (coming soon...) ---
 
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// ----- DO NOT EDIT BELOW THIS POINT ------
 
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}
 
}
 
}}
 
}}

Latest revision as of 11:00, 13 October 2024

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
	CoMOffset = -0.7, -0.6, 0
	CoLOffset = -0.7, -0.6, 0
	CoPOffset = -0.7, -0.6, 0
	TechRequired = supersonicFlight
	entryCost = 6400
	cost = 500
	category = Aero
	subcategory = 0
	title = #autoLOC_500268 //#autoLOC_500268 = Structural Wing Type A
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500269 //#autoLOC_500269 = 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
	tags = #autoLOC_500270 //#autoLOC_500270 = aero aircraft fligh foil lift plane swept
	MODEL
	{
		model = Squad/Parts/Aero/wings/structural1
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 1
		dragAtMaxAoA = 0.3
		dragAtMinAoA = 0.0
	}
	MODULE
	{
		name = ModuleCargoPart		
		packedVolume = -1
	}
}
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