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

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m (*update to 1.0.4;)
m (Update config)
 
Line 1: Line 1:
{{Part config|Ram Air Intake|2=PART
+
{{Part config|Adjustable Ramp Intake|2=PART
 
{
 
{
 
name = ramAirIntake
 
name = ramAirIntake
Line 7: Line 7:
 
rescaleFactor = 1
 
rescaleFactor = 1
 
node_stack_bottom01 = 0.0, 0.0, 0.0, 0.0, -1.0, 0.0
 
node_stack_bottom01 = 0.0, 0.0, 0.0, 0.0, -1.0, 0.0
TechRequired = supersonicFlight
+
buoyancy = 0.1
 +
TechRequired = highAltitudeFlight
 
entryCost = 14000
 
entryCost = 14000
 
cost = 2680
 
cost = 2680
 
category = Aero
 
category = Aero
 
subcategory = 0
 
subcategory = 0
title = Ram Air Intake
+
title = #autoLOC_500202 //#autoLOC_500202 = Adjustable Ramp Intake
manufacturer = C7 Aerospace Division
+
manufacturer = #autoLOC_501624 //#autoLOC_501624 = 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.
+
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
 
attachRules = 1,0,1,1,0
 
stackSymmetry = 2
 
stackSymmetry = 2
mass = 0.01
+
mass = 0.06
 
thermalMassModifier = 12.0
 
thermalMassModifier = 12.0
 
// heatConductivity = 0.06 // half default
 
// heatConductivity = 0.06 // half default
Line 29: Line 30:
 
fuelCrossFeed = True
 
fuelCrossFeed = True
 
bulkheadProfiles = size1
 
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
 
MODULE
 
{
 
{
Line 34: Line 40:
 
resourceName = IntakeAir
 
resourceName = IntakeAir
 
checkForOxygen = true
 
checkForOxygen = true
area = 0.01
+
area = 0.0074
 
intakeSpeed = 10
 
intakeSpeed = 10
 
intakeTransformName = Intake
 
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
 
RESOURCE
 
{
 
{
 
name = IntakeAir
 
name = IntakeAir
amount = 1.0
+
amount = 2
maxAmount = 1.0
+
maxAmount = 2
 
}
 
}
 
MODULE
 
MODULE
Line 48: Line 62:
 
name = ModuleAnimateHeat
 
name = ModuleAnimateHeat
 
ThermalAnim = IntakeRampHeat
 
ThermalAnim = IntakeRampHeat
 +
}
 +
MODULE
 +
{
 +
name = ModuleCargoPart
 +
stackableQuantity = 1
 +
packedVolume = -1
 
}
 
}
 
}
 
}
 
 
}}
 
}}

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
	}
}