Difference between revisions of "Parts/Aero/cones/smallNoseCone.cfg"

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(Created page with "<pre> // this is a sample config file, for determining a good file format for defining part parameters // comment line - ignored by cfg parser // empty lines, or lines without...")
 
(Updated for 0.23)
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<pre>
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{{Part config|Standard NC|2=PART
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{
 
// this is a sample config file, for determining a good file format for defining part parameters
 
// this is a sample config file, for determining a good file format for defining part parameters
 
// comment line - ignored by cfg parser
 
// comment line - ignored by cfg parser
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// --- editor parameters ---
 
// --- editor parameters ---
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TechRequired = advAerodynamics
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entryCost = 6800
 
cost = 680
 
cost = 680
 
category = Aero
 
category = Aero
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// ----- DO NOT EDIT BELOW THIS POINT ------
 
// ----- DO NOT EDIT BELOW THIS POINT ------
</pre>
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}
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}}

Revision as of 12:49, 24 January 2014

This is the configuration file for Standard NC.
PART
{
// this is a sample config file, for determining a good file format for defining part parameters
// comment line - ignored by cfg parser
// empty lines, or lines without a '=' sign are also ignored
// all other lines are split at the '=' sign, and the left operand is used to know what parameter we are setting
// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
// 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)


// --- general parameters ---
name = standardNoseCone
module = Strut
author = C. Jenkins

// --- asset parameters ---
mesh = model.mu
scale = 1.0

// --- node definitions ---
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z

node_stack_bottom01 = 0.0, -0.138, 0.0, 0.0, 1.0, 0.0



// --- FX definitions ---


// --- editor parameters ---
TechRequired = advAerodynamics
entryCost = 6800
cost = 680
category = Aero
subcategory = 0
title = Standard NC
manufacturer = C7 Aerospace Division.
description = An aerodynamic nose cap. 

// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
attachRules = 1,0,1,0,0
stackSymmetry = 2

// --- standard part parameters ---
mass = 0.1
dragModelType = default
maximum_drag = 0.1
minimum_drag = 0.1
angularDrag = .25
crashTolerance = 40
maxTemp = 3400
fuelCrossFeed = True

// ----- DO NOT EDIT BELOW THIS POINT ------
}