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

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m (corrected mass from 0.01 to 0.011)
m (Update config)
 
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{{Part config|Ram Air Intake|2=PART
+
{{Part config|Adjustable Ramp Intake|2=PART
 
{
 
{
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// this is a sample config file, for determining a good file format for defining part parameters
+
name = ramAirIntake
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// comment line - ignored by cfg parser
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module = Part
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// empty lines, or lines without a '=' sign are also ignored
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author = C. Jenkins, Porkjet
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// all other lines are split at the '=' sign, and the left operand is used to know what parameter we are setting
+
mesh = RampIntake.mu
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// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
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rescaleFactor = 1
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// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
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node_stack_bottom01 = 0.0, 0.0, 0.0, 0.0, -1.0, 0.0
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// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
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buoyancy = 0.1
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// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
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TechRequired = highAltitudeFlight
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// 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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entryCost = 14000
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cost = 2680
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category = Aero
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// --- general parameters ---
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subcategory = 0
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name = ramAirIntake
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title = #autoLOC_500202 //#autoLOC_500202 = Adjustable Ramp Intake
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module = Part
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manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
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author = C. Jenkins
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description = #autoLOC_500203 //#autoLOC_500203 = 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 efficiency of this unit at supersonic speeds. Patents Pending.
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+
attachRules = 1,0,1,1,0
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// --- asset parameters ---
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stackSymmetry = 2
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mesh = model.mu
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mass = 0.06
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scale = 0.1
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thermalMassModifier = 12.0
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// heatConductivity = 0.06 // half default
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// --- node definitions ---
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emissiveConstant = 0.7
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// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
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dragModelType = default
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maximum_drag = 0.3
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node_stack_bottom01 = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0
+
minimum_drag = 0.3
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angularDrag = 1
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crashTolerance = 7
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maxTemp = 2400 // = 3400
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// --- FX definitions ---
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fuelCrossFeed = True
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bulkheadProfiles = size1
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tags = #autoLOC_500204 //#autoLOC_500204 = aero (air aircraft breathe cone fligh inlet jet oxygen plane suck supersonic
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// --- editor parameters ---
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DRAG_CUBE
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TechRequired = highAltitudeFlight
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{
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entryCost = 14000
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cube = Default, 1.455778,0.8035793,0.7221571, 1.455778,0.8028867,0.7221571, 1.218224,0.375,1.891716, 1.218224,0.9445066,1.006232, 1.975862,0.8134198,1.148628, 1.975862,0.8425881,0.7164711, -3.725912E-08,0.8638564,3.089391E-07, 1.25,1.852713,1.250001
−
cost = 2680
+
}
−
category = Aero
+
MODULE
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subcategory = 0
+
{
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title = Ram Air Intake
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name = ModuleResourceIntake
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manufacturer = C7 Aerospace Division
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resourceName = IntakeAir
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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.
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checkForOxygen = true
−
 
+
area = 0.0074
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+
intakeSpeed = 10
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intakeTransformName = Intake
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// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
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machCurve
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attachRules = 1,0,1,0,0
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{
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stackSymmetry = 2
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key = 0 0.85 0 0
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key = 1 1 0 0
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// --- standard part parameters ---
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key = 2 0.95 -0.08751557 -0.08751557
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mass = 0.011
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key = 4 0.5 -0.4034287 -0.4034287
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dragModelType = default
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key = 8 0.01 0 0
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maximum_drag = 0.3
+
}
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minimum_drag = 0.3
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}
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angularDrag = 1
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RESOURCE
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crashTolerance = 10
+
{
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maxTemp = 3400
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name = IntakeAir
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fuelCrossFeed = True
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amount = 2
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maxAmount = 2
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+
}
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// ----- DO NOT EDIT BELOW THIS POINT ------
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MODULE
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+
{
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MODULE
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name = ModuleAnimateHeat
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{
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ThermalAnim = IntakeRampHeat
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  name = ModuleResourceIntake
+
}
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  resourceName = IntakeAir
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MODULE
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  checkForOxygen = true
+
{
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  area = 0.01
+
name = ModuleCargoPart
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  intakeSpeed = 10
+
stackableQuantity = 1
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  intakeTransformName = Intake
+
packedVolume = -1
−
}
+
}
−
 
 
−
RESOURCE
 
−
{
 
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name = IntakeAir
 
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amount = 0.2
 
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maxAmount = 0.2
 
−
}
 
 
}
 
}
−
 
 
}}
 
}}

Latest revision as of 10:51, 13 October 2024

This is the configuration file for Adjustable Ramp 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
	buoyancy = 0.1
	TechRequired = highAltitudeFlight
	entryCost = 14000
	cost = 2680
	category = Aero
	subcategory = 0
	title = #autoLOC_500202 //#autoLOC_500202 = Adjustable Ramp Intake
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500203 //#autoLOC_500203 = 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 efficiency of this unit at supersonic speeds. Patents Pending.
	attachRules = 1,0,1,1,0
	stackSymmetry = 2
	mass = 0.06
	thermalMassModifier = 12.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.7
	dragModelType = default
	maximum_drag = 0.3
	minimum_drag = 0.3
	angularDrag = 1
	crashTolerance = 7
	maxTemp = 2400 // = 3400
	fuelCrossFeed = True
	bulkheadProfiles = size1
	tags = #autoLOC_500204 //#autoLOC_500204 = aero (air aircraft breathe cone fligh inlet jet oxygen plane suck supersonic
	DRAG_CUBE
	{
		cube = Default, 1.455778,0.8035793,0.7221571, 1.455778,0.8028867,0.7221571, 1.218224,0.375,1.891716, 1.218224,0.9445066,1.006232, 1.975862,0.8134198,1.148628, 1.975862,0.8425881,0.7164711, -3.725912E-08,0.8638564,3.089391E-07, 1.25,1.852713,1.250001
	}
	MODULE
	{
		name = ModuleResourceIntake
		resourceName = IntakeAir
		checkForOxygen = true
		area = 0.0074
		intakeSpeed = 10
		intakeTransformName = Intake
		machCurve
		{
			key = 0 0.85 0 0
			key = 1 1 0 0
			key = 2 0.95 -0.08751557 -0.08751557
			key = 4 0.5 -0.4034287 -0.4034287
			key = 8 0.01 0 0
		}
	}
	RESOURCE
	{
		name = IntakeAir
		amount = 2
		maxAmount = 2
	}
	MODULE
	{
		name = ModuleAnimateHeat
		ThermalAnim = IntakeRampHeat
	}	
	MODULE
	{
		name = ModuleCargoPart	
		stackableQuantity = 1
		packedVolume = -1
	}
}
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