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

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m (BobBot moved page Parts/noseConeAdapter/part.cfg to Parts/Aero/noseConeAdapter/part.cfg without leaving a redirect: Update to new directory system)
m (*update to 1.0.4;)
 
(5 intermediate revisions by the same user not shown)
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{{Part config|NCS Adapter|2=PART
 
{{Part config|NCS Adapter|2=PART
 
{
 
{
// this is a sample config file, for determining a good file format for defining part parameters
+
name = noseConeAdapter
// comment line - ignored by cfg parser
+
module = Part
// empty lines, or lines without a '=' sign are also ignored
+
author = C. Jenkins, 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_stack_top = 0.0, 1.125, 0.0, 0.0, 1.0, 0.0, 0
// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
+
node_stack_bottom01 = 0.0, -0.75, 0.0, 0.0, -1.0, 0.0, 1
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
node_attach = 0, 0, -0.313, 0.0, 0.0, 1.0
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
TechRequired = advAerodynamics
// 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 = 6500
 
+
cost = 320
 
+
category = Propulsion
// --- general parameters ---
+
subcategory = 0
name = noseConeAdapter
+
title = NCS Adapter
module = Part
+
manufacturer = C7 Aerospace Division
author = C. Jenkins
+
description = The base of C7 Aerospace's Nose Cone system (NCS)
 
+
attachRules = 1,1,1,1,0
// --- asset parameters ---
+
mass = 0.1
mesh = model.mu
+
dragModelType = default
scale = 1.0
+
maximum_drag = 0.1
 
+
minimum_drag = 0.1
 
+
angularDrag = 1
// --- node definitions ---
+
crashTolerance = 20
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
+
maxTemp = 2400
node_stack_top = 0.0, 0.555, 0.0, 0.0, 1.0, 0.0
+
thermalMassModifier = 6.0
node_stack_bottom01 = 0.0, -0.440, 0.0, 0.0, 1.0, 0.0
+
emissiveConstant = 0.95
 
+
fuelCrossFeed = True
 +
bulkheadProfiles = size0, size1
 +
MODEL
 +
{
 +
model = Squad/Parts/Aero/cones/NCS
 +
}
 +
RESOURCE
 +
{
 +
name = LiquidFuel
 +
amount = 80
 +
maxAmount = 80
 +
}
 +
MODULE
 +
{
 +
name = ModuleAnimateHeat
 +
ThermalAnim = Cone_Heat
 +
}
 +
}
  
 
// --- FX definitions ---
 
 
 
// --- editor parameters ---
 
TechRequired = advAerodynamics
 
entryCost = 6500
 
cost = 680
 
category = Structural
 
subcategory = 0
 
title = NCS Adapter
 
manufacturer = C7 Aerospace Division.
 
description = The base of C7 Aerospace's Nose Cone system (NCS)
 
 
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
 
attachRules = 1,0,1,1,0
 
stackSymmetry = 2
 
 
// --- standard part parameters ---
 
mass = 0.3
 
dragModelType = default
 
maximum_drag = 0.1
 
minimum_drag = 0.1
 
angularDrag = 1
 
crashTolerance = 20
 
maxTemp = 3400
 
fuelCrossFeed = True
 
 
 
// ----- DO NOT EDIT BELOW THIS POINT ------
 
}
 
 
}}
 
}}

Latest revision as of 12:13, 27 June 2015

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
	TechRequired = advAerodynamics
	entryCost = 6500
	cost = 320
	category = Propulsion
	subcategory = 0
	title = NCS Adapter
	manufacturer = C7 Aerospace Division
	description = 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 = 20
	maxTemp = 2400
	thermalMassModifier = 6.0
	emissiveConstant = 0.95
	fuelCrossFeed = True
	bulkheadProfiles = size0, size1
	MODEL
	{
		model = Squad/Parts/Aero/cones/NCS
	}
	RESOURCE
	{
		name = LiquidFuel
		amount = 80
		maxAmount = 80
	}
	MODULE
	{
		name = ModuleAnimateHeat
		ThermalAnim = Cone_Heat
	}
}