Difference between revisions of "Parts/Aero/wingletAV-T1/wingletAV-T1.cfg"

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<pre>
+
{{Part config|AV-T1 Winglet|2=PART
// this is a sample config file, for determining a good file format for defining part parameters
+
{
// comment line - ignored by cfg parser
+
name = winglet
// empty lines, or lines without a '=' sign are also ignored
+
module = Part
// all other lines are split at the '=' sign, and the left operand is used to know what parameter we are setting
+
author = HarvesteR
// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
+
mesh = model.mu
// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
+
scale = 0.1
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
TechRequired = stability
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
entryCost = 1500
// 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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cost = 500
 
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category = Aero
 
+
subcategory = 0
// --- general parameters ---
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title = #autoLOC_500223 //#autoLOC_500223 = AV-T1 Winglet
name = winglet
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description = #autoLOC_500224 //#autoLOC_500224 = Nothing is really known about this thing. Use it at your own risk.
module = Winglet
+
attachRules = 0,1,0,0,1
author = HarvesteR
+
node_attach = 5.10736, -0.589634, 0.0, 1.0, 0.0, 0.0
 
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CoMOffset = 0.08, -0.2, 0.00664
// --- asset parameters ---
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CoLOffset = 0.08, -0.2, 0.00664
mesh = model.mu
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CoPOffset = 0.08, -0.2, 0.00664
scale = 0.1
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mass = 0.037
 
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thermalMassModifier = 8.0
 
+
// heatConductivity = 0.06 // half default
// --- editor parameters ---
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emissiveConstant = 0.95
cost = 500
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dragModelType = none
category = Aero
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maximum_drag = 0.02
subcategory = 0
+
minimum_drag = 0.02
title = AV-T1 Winglet
+
angularDrag = 5
// manufacturer = Kerlington Model Rockets and Paper Products Inc.
+
crashTolerance = 12
// description =
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maxTemp = 2400
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
explosionPotential = 0.1
attachRules = 0,1,0,0,1
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mirrorRefAxis = 0, 0, -1
 
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bulkheadProfiles = srf
// --- node definitions ---
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tags = #autoLOC_500225 //#autoLOC_500225 = aero aircraft fin lift plane rocket stab swept
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
+
MODULE
node_attach = 5.10736, -0.589634, 0.0, 1.0, 0.0, 0.0
+
{
 
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name = ModuleLiftingSurface
 
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useInternalDragModel = True
// --- standard part parameters ---
+
deflectionLiftCoeff = 0.37
mass = 0.05
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dragAtMaxAoA = 0.3
dragModelType = override
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}
maximum_drag = 0.02
+
MODULE
minimum_drag = 0.02
+
{
angularDrag = 5
+
name = ModuleCargoPart
crashTolerance = 12
+
packedVolume = 400
maxTemp = 3400
+
}
explosionPotential = 0.1
+
}
 
+
}}
mirrorRefAxis = 0, 0, -1
 
 
 
// --- winglet parameters ---
 
// dragCoeff will override the maximum_drag value
 
dragCoeff = 0.5
 
deflectionLiftCoeff = 0.3
 
 
 
 
 
 
 
// --- tweakables (coming soon...) ---
 
 
 
 
 
 
 
 
 
// ----- DO NOT EDIT BELOW THIS POINT ------
 
</pre>
 

Latest revision as of 11:10, 13 October 2024

This is the configuration file for AV-T1 Winglet.
PART
{
	name = winglet
	module = Part
	author = HarvesteR
	mesh = model.mu
	scale = 0.1
	TechRequired = stability
	entryCost = 1500
	cost = 500
	category = Aero
	subcategory = 0
	title = #autoLOC_500223 //#autoLOC_500223 = AV-T1 Winglet
	description = #autoLOC_500224 //#autoLOC_500224 = Nothing is really known about this thing. Use it at your own risk.
	attachRules = 0,1,0,0,1
	node_attach = 5.10736, -0.589634, 0.0, 1.0, 0.0, 0.0
	CoMOffset = 0.08, -0.2, 0.00664
	CoLOffset = 0.08, -0.2, 0.00664
	CoPOffset = 0.08, -0.2, 0.00664
	mass = 0.037
	thermalMassModifier = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 5
	crashTolerance = 12
	maxTemp = 2400
	explosionPotential = 0.1
	mirrorRefAxis = 0, 0, -1
	bulkheadProfiles = srf
	tags = #autoLOC_500225 //#autoLOC_500225 = aero aircraft fin lift plane rocket stab swept
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 0.37
		dragAtMaxAoA = 0.3
	}
	MODULE
	{
		name = ModuleCargoPart
		packedVolume = 400
	}
}