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

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m (*update to 0.24.2;)
m (*update to 1.0.4;)
 
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{{Part config|Delta Wing|2=PART
 
{{Part config|Delta Wing|2=PART
 
{
 
{
// this is a sample config file, for determining a good file format for defining part parameters
+
name = deltaWing
// comment line - ignored by cfg parser
+
module = Part
// empty lines, or lines without a '=' sign are also ignored
+
author = Porkjet
// all other lines are split at the '=' sign, and the left operand is used to know what parameter we are setting
+
rescaleFactor = 1
// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
+
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
+
CoLOffset = -1.2, 0.4, 0
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
CoPOffset = -1.2, 0.4, 0
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
TechRequired = aerodynamicSystems
// 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)
+
entryCost = 6400
 
+
cost = 600
 
+
category = Aero
// --- general parameters ---
+
subcategory = 0
name = deltaWing
+
title = Delta Wing
module = Winglet
+
manufacturer = C7 Aerospace Division
author = C. Jenkins
+
description = Standard Delta configuration wings. These wings provide high lift and a stable center of gravity for your everyday lifting needs.
 
+
attachRules = 0,1,0,1,1
// --- asset parameters ---
+
mass = 0.2
mesh = c7deltawing.DAE
+
thermalMassModifier = 8.0
scale = 0.1
+
// heatConductivity = 0.06 // half default
 
+
emissiveConstant = 0.95
// --- editor parameters ---
+
dragModelType = none
TechRequired = supersonicFlight
+
maximum_drag = 0.02
entryCost = 5400
+
minimum_drag = 0.02
cost = 680
+
angularDrag = 2
category = Aero
+
crashTolerance = 15
subcategory = 0
+
maxTemp = 2400
title = Delta Wing
+
explosionPotential = 0.1
manufacturer = C7 Aerospace Division
+
fuelCrossFeed = True
description = Standard Delta configuration wings. These wings provide high lift and a stable center of gravity for your everyday lifting needs.
+
bulkheadProfiles = srf
 
+
MODEL
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
{
attachRules = 0,1,0,1,1
+
model = Squad/Parts/Aero/wings/delta
 
+
}
// --- node definitions ---
+
MODULE
// 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
+
name = ModuleLiftingSurface
 
+
useInternalDragModel = True
 
+
deflectionLiftCoeff = 2.0
// --- standard part parameters ---
+
dragAtMaxAoA = 0.6
mass = 0.07
+
dragAtMinAoA = 0.0
dragModelType = override
+
}
maximum_drag = 0.02
 
minimum_drag = 0.02
 
angularDrag = 2
 
crashTolerance = 15
 
maxTemp = 3400
 
explosionPotential = 0.1
 
fuelCrossFeed = True
 
// --- winglet parameters ---
 
// dragCoeff will override the maximum_drag value
 
dragCoeff = 0.6
 
deflectionLiftCoeff = 1.9
 
 
 
 
 
 
 
// --- tweakables (coming soon...) ---
 
 
 
 
 
 
 
 
 
// ----- DO NOT EDIT BELOW THIS POINT ------
 
 
 
 
}
 
}
  
 
}}
 
}}

Latest revision as of 12:11, 27 June 2015

This is the configuration file for Delta Wing.
PART
{
	name = deltaWing
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	CoLOffset = -1.2, 0.4, 0
	CoPOffset = -1.2, 0.4, 0
	TechRequired = aerodynamicSystems
	entryCost = 6400
	cost = 600
	category = Aero
	subcategory = 0
	title = Delta Wing
	manufacturer = C7 Aerospace Division
	description = Standard Delta configuration wings. These wings provide high lift and a stable center of gravity for your everyday lifting needs.
	attachRules = 0,1,0,1,1
	mass = 0.2
	thermalMassModifier = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 2
	crashTolerance = 15
	maxTemp = 2400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	MODEL
	{
		model = Squad/Parts/Aero/wings/delta
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 2.0
		dragAtMaxAoA = 0.6
		dragAtMinAoA = 0.0
	}
}