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

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<pre>
+
{{Part config|NCS Adapter|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 = noseConeAdapter
// 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 = C. Jenkins, 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_stack_top = 0.0, 1.125, 0.0, 0.0, 1.0, 0.0, 0
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
node_stack_bottom01 = 0.0, -0.75, 0.0, 0.0, -1.0, 0.0, 1
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
node_attach = 0, 0, -0.313, 0.0, 0.0, 1.0
// 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)
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CenterOfDisplacement = 0.0, -0.2, 0.0
 
+
TechRequired = aerodynamicSystems
 
+
entryCost = 6500
// --- general parameters ---
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cost = 320
name = noseConeAdapter
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category = Propulsion
module = Strut
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subcategory = 0
author = C. Jenkins
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title = #autoLOC_500157 //#autoLOC_500157 = NCS Adapter
 
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manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
// --- asset parameters ---
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description = #autoLOC_500158 //#autoLOC_500158 = The base of C7 Aerospace's Nose Cone system (NCS)
mesh = model.mu
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attachRules = 1,1,1,1,0
scale = 1.0
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mass = 0.1
 
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dragModelType = default
 
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maximum_drag = 0.1
// --- node definitions ---
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minimum_drag = 0.1
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
+
angularDrag = 1
node_stack_top = 0.0, 0.555, 0.0, 0.0, 1.0, 0.0
+
crashTolerance = 10
node_stack_bottom01 = 0.0, -0.440, 0.0, 0.0, 1.0, 0.0
+
maxTemp = 2400
 
+
thermalMassModifier = 6.0
 
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emissiveConstant = 0.95
 
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tags = #autoLOC_500159 //#autoLOC_500159 = aero aircraft booster )cap cone drag fligh nose plane rocket stab stream tail
// --- FX definitions ---
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fuelCrossFeed = True
 
+
bulkheadProfiles = size0, size1
 
+
MODEL
// --- editor parameters ---
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{
cost = 680
+
model = Squad/Parts/Aero/cones/Assets/NCS
category = Structural
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}
subcategory = 0
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RESOURCE
title = NCS Adapter
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{
manufacturer = C7 Aerospace Division.
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name = LiquidFuel
description = The base of C7 Aerospace's Nose Cone system (NCS)
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amount = 80
 
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maxAmount = 80
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
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}
attachRules = 1,0,1,1,0
+
MODULE
stackSymmetry = 2
+
{
 
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name = ModuleAnimateHeat
// --- standard part parameters ---
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ThermalAnim = Cone_Heat
mass = 0.3
+
}
dragModelType = default
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}
maximum_drag = 0.3
+
}}
minimum_drag = 0.3
 
angularDrag = 1
 
crashTolerance = 20
 
maxTemp = 3400
 
fuelCrossFeed = True
 
 
 
 
 
// ----- DO NOT EDIT BELOW THIS POINT ------
 
</pre>
 

Latest revision as of 15:50, 10 October 2024

This is the configuration file for NCS Adapter.
PART
{
	name = noseConeAdapter
	module = Part
	author = C. Jenkins, Porkjet
	rescaleFactor = 1
	node_stack_top = 0.0, 1.125, 0.0, 0.0, 1.0, 0.0, 0
	node_stack_bottom01 = 0.0, -0.75, 0.0, 0.0, -1.0, 0.0, 1
	node_attach = 0, 0, -0.313, 0.0, 0.0, 1.0
	CenterOfDisplacement = 0.0, -0.2, 0.0
	TechRequired = aerodynamicSystems
	entryCost = 6500
	cost = 320
	category = Propulsion
	subcategory = 0
	title = #autoLOC_500157 //#autoLOC_500157 = NCS Adapter
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500158 //#autoLOC_500158 = The base of C7 Aerospace's Nose Cone system (NCS)
	attachRules = 1,1,1,1,0
	mass = 0.1
	dragModelType = default
	maximum_drag = 0.1
	minimum_drag = 0.1
	angularDrag = 1
	crashTolerance = 10
	maxTemp = 2400
	thermalMassModifier = 6.0
	emissiveConstant = 0.95
	tags = #autoLOC_500159 //#autoLOC_500159 = aero aircraft booster )cap cone drag fligh nose plane rocket stab stream tail
	fuelCrossFeed = True
	bulkheadProfiles = size0, size1
	MODEL
	{
		model = Squad/Parts/Aero/cones/Assets/NCS
	}
	RESOURCE
	{
		name = LiquidFuel
		amount = 80
		maxAmount = 80
	}
	MODULE
	{
		name = ModuleAnimateHeat
		ThermalAnim = Cone_Heat
	}
}