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

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<pre>
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{{Part config|Structural Wing Type A|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 = structuralWing
// 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 = Porkjet
// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
+
rescaleFactor = 1
// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
+
node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
CoLOffset = -0.7, -0.6, 0
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
CoPOffset = -0.7, -0.6, 0
// 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)
+
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
 +
}
 +
}
  
 
+
}}
// --- general parameters ---
 
name = structuralWing
 
module = Winglet
 
author = C. Jenkins
 
 
 
// --- asset parameters ---
 
mesh = model.mu
 
scale = 0.1
 
 
 
// --- editor parameters ---
 
cost = 500
 
category = Aero
 
subcategory = 0
 
title = Structural Wing
 
manufacturer = C7 Aerospace division
 
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.
 
 
 
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
 
attachRules = 0,1,0,1,1
 
 
 
// --- node definitions ---
 
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
 
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0
 
 
 
 
 
// --- standard part parameters ---
 
mass = 0.05
 
dragModelType = override
 
maximum_drag = 0.02
 
minimum_drag = 0.02
 
angularDrag = 2
 
crashTolerance = 15
 
maxTemp = 3400
 
explosionPotential = 0.1
 
fuelCrossFeed = True
 
breakingTorque = 100
 
// --- winglet parameters ---
 
// dragCoeff will override the maximum_drag value
 
dragCoeff = 0.4
 
deflectionLiftCoeff = 1.0
 
 
 
 
 
 
 
// --- tweakables (coming soon...) ---
 
 
 
 
 
 
 
 
 
// ----- DO NOT EDIT BELOW THIS POINT ------
 
</pre>
 

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
	}
}