Difference between revisions of "Parts/Aero/ramAirIntake/ramAirIntake.cfg"

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m (BobBot moved page Parts/Utility/ramAirIntake/ramAirIntake.cfg to Parts/Aero/ramAirIntake/ramAirIntake.cfg without leaving a redirect: Renamed part configuration file after update.)
m (*update to 1.0;)
Line 1: Line 1:
 
{{Part config|Ram Air Intake|2=PART
 
{{Part config|Ram Air Intake|2=PART
 
{
 
{
−
// this is a sample config file, for determining a good file format for defining part parameters
+
name = ramAirIntake
−
// 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
+
mesh = RampIntake.mu
−
// 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_bottom01 = 0.0, 0.0, 0.0, 0.0, -1.0, 0.0
−
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
TechRequired = supersonicFlight
−
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
entryCost = 14000
−
// 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)
+
cost = 2680
−
 
+
category = Aero
−
 
+
subcategory = 0
−
// --- general parameters ---
+
title = Ram Air Intake
−
name = ramAirIntake
+
manufacturer = C7 Aerospace Division
−
module = Part
+
description = At supersonic speeds, -PATENT PENDING, CLASSIFIED INFO- inside the intake duct deflect the incoming air stream, causing -PATENT PENDING, CLASSIFIED INFO-, which creates a -PATENT PENDING, CLASSIFIED INFO-, thereby greatly increasing the efficency of this unit at high altitudes and speeds. Patents Pending.
−
author = C. Jenkins
+
attachRules = 1,0,1,1,0
−
 
+
stackSymmetry = 2
−
// --- asset parameters ---
+
mass = 0.01
−
mesh = model.mu
+
thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K
−
scale = 0.1
+
// heatConductivity = 0.06 // half default
−
 
+
emissiveConstant = 0.7
−
// --- node definitions ---
+
dragModelType = default
−
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
+
maximum_drag = 0.3
−
 
+
minimum_drag = 0.3
−
node_stack_bottom01 = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0
+
angularDrag = 1
−
 
+
crashTolerance = 7
−
 
+
maxTemp = 2100 // = 3400
−
 
+
fuelCrossFeed = True
−
// --- FX definitions ---
+
bulkheadProfiles = size1
−
 
+
MODULE
−
 
+
{
−
// --- editor parameters ---
+
name = ModuleResourceIntake
−
TechRequired = highAltitudeFlight
+
resourceName = IntakeAir
−
entryCost = 14000
+
checkForOxygen = true
−
cost = 2680
+
area = 0.01
−
category = Aero
+
intakeSpeed = 10
−
subcategory = 0
+
intakeTransformName = Intake
−
title = Ram Air Intake
+
}
−
manufacturer = C7 Aerospace Division
+
RESOURCE
−
description = Not your average air intake. These High Performance air intakes have their own pre-compressors, to supercharge air-breathing engines at very high altitudes.
+
{
−
 
+
name = IntakeAir
−
 
+
amount = 1.0
−
 
+
maxAmount = 1.0
−
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
}
−
attachRules = 1,0,1,0,0
 
−
stackSymmetry = 2
 
−
 
 
−
// --- standard part parameters ---
 
−
mass = 0.01
 
−
dragModelType = default
 
−
maximum_drag = 0.3
 
−
minimum_drag = 0.3
 
−
angularDrag = 1
 
−
crashTolerance = 10
 
−
maxTemp = 3400
 
−
fuelCrossFeed = True
 
−
 
 
−
 
 
−
// ----- DO NOT EDIT BELOW THIS POINT ------
 
−
 
 
−
MODULE
 
−
{
 
−
  name = ModuleResourceIntake
 
−
  resourceName = IntakeAir
 
−
  checkForOxygen = true
 
−
  area = 0.01
 
−
  intakeSpeed = 10
 
−
  intakeTransformName = Intake
 
−
}
 
−
 
 
−
RESOURCE
 
−
{
 
−
name = IntakeAir
 
−
amount = 0.2
 
−
maxAmount = 0.2
 
−
}
 
 
}
 
}
  
 
}}
 
}}

Revision as of 13:11, 29 April 2015

This is the configuration file for Ram Air Intake. 
PART
{
	name = ramAirIntake
	module = Part
	author = C. Jenkins, Porkjet
	mesh = RampIntake.mu
	rescaleFactor = 1
	node_stack_bottom01 = 0.0, 0.0, 0.0, 0.0, -1.0, 0.0
	TechRequired = supersonicFlight
	entryCost = 14000
	cost = 2680
	category = Aero
	subcategory = 0
	title = Ram Air Intake
	manufacturer = C7 Aerospace Division
	description = At supersonic speeds, -PATENT PENDING, CLASSIFIED INFO- inside the intake duct deflect the incoming air stream, causing -PATENT PENDING, CLASSIFIED INFO-, which creates a -PATENT PENDING, CLASSIFIED INFO-, thereby greatly increasing the efficency of this unit at high altitudes and speeds. Patents Pending.
	attachRules = 1,0,1,1,0
	stackSymmetry = 2
	mass = 0.01
	thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.7
	dragModelType = default
	maximum_drag = 0.3
	minimum_drag = 0.3
	angularDrag = 1
	crashTolerance = 7
	maxTemp = 2100 // = 3400
	fuelCrossFeed = True
	bulkheadProfiles = size1
	MODULE
	{
		name = ModuleResourceIntake
		resourceName = IntakeAir
		checkForOxygen = true
		area = 0.01
		intakeSpeed = 10
		intakeTransformName = Intake
	}
	RESOURCE
	{
		name = IntakeAir
		amount = 1.0
		maxAmount = 1.0
	}
}
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