Difference between revisions of "Parts/Aero/airIntakeRadialXM-G50/airIntakeRadialXM-G50.cfg"

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m (*update to 1.0.4;)
m (Update config)
 
Line 3: Line 3:
 
name = airScoop
 
name = airScoop
 
module = Part
 
module = Part
author = NovaSilisko
+
author = NovaSilisko, Porkjet
mesh = model.mu
+
mesh = RadialIntake.mu
 
rescaleFactor = 1
 
rescaleFactor = 1
 
node_attach = 0.0, 0.3370661, 0.0, 0.0, 1.0, 0.0
 
node_attach = 0.0, 0.3370661, 0.0, 0.0, 1.0, 0.0
TechRequired = aviation
+
buoyancy = 0.1
entryCost = 4500
+
TechRequired = aerodynamicSystems
cost = 1000
+
entryCost = 2500
 +
cost = 250
 
category = Aero
 
category = Aero
 
subcategory = 0
 
subcategory = 0
title = XM-G50 Radial Air Intake
+
title = #autoLOC_500115 //#autoLOC_500115 = XM-G50 Radial Air Intake
manufacturer = Vac-Co Advanced Suction Systems
+
manufacturer = #autoLOC_501625 //#autoLOC_501625 = Vac-Co Advanced Suction Systems
description = A must-have for air breathing engines, this intake duct will pull in outside air to run turbine engines on, as long as there is any outside air to begin with, of course. Warranty does not cover engine flame-outs or any objects, inanimate or otherwise, sucked in by the intake.
+
description = #autoLOC_500116 //#autoLOC_500116 = An intake duct version that can be mounted at the sides of a fuselage. Warranty does not cover engine flame-outs or any objects, inanimate or otherwise, sucked in by the intake. Optimized for subsonic flight.
 
attachRules = 0,1,0,0,0
 
attachRules = 0,1,0,0,0
mass = 0.01
+
mass = 0.02
 
thermalMassModifier = 6.0
 
thermalMassModifier = 6.0
 
// heatConductivity = 0.06 // half default
 
// heatConductivity = 0.06 // half default
Line 23: Line 24:
 
minimum_drag = 0.2
 
minimum_drag = 0.2
 
angularDrag = 1
 
angularDrag = 1
crashTolerance = 80
+
crashTolerance = 10
 
breakingForce = 200
 
breakingForce = 200
 
breakingTorque = 200
 
breakingTorque = 200
 
maxTemp = 2000
 
maxTemp = 2000
 
bulkheadProfiles = srf
 
bulkheadProfiles = srf
 +
tags = #autoLOC_500117 //#autoLOC_500117 = aero aircraft breathe fligh inlet jet oxygen plane subsonic suck
 
MODULE
 
MODULE
 
{
 
{
Line 33: Line 35:
 
resourceName = IntakeAir
 
resourceName = IntakeAir
 
checkForOxygen = true
 
checkForOxygen = true
area = 0.006
+
area = 0.0031
intakeSpeed = 10
+
intakeSpeed = 15
 
intakeTransformName = Intake
 
intakeTransformName = Intake
 +
machCurve
 +
{
 +
key = 1 1 0 0
 +
key = 1.5 0.9 -0.4312553 -0.4312553
 +
key = 2.5 0.45 -0.5275364 -0.5275364
 +
key = 3.5 0.1 0 0
 +
}
 
}
 
}
 
RESOURCE
 
RESOURCE
 
{
 
{
 
name = IntakeAir
 
name = IntakeAir
amount = 0.6
+
amount = 2
maxAmount = 0.6
+
maxAmount = 2
 +
}
 +
MODULE
 +
{
 +
name = ModuleCargoPart
 +
packedVolume = 2250
 
}
 
}
 
}
 
}
 
 
}}
 
}}

Latest revision as of 10:54, 13 October 2024

This is the configuration file for XM-G50 Radial Air Intake.
PART
{
	name = airScoop
	module = Part
	author = NovaSilisko, Porkjet
	mesh = RadialIntake.mu
	rescaleFactor = 1
	node_attach = 0.0, 0.3370661, 0.0, 0.0, 1.0, 0.0
	buoyancy = 0.1
	TechRequired = aerodynamicSystems
	entryCost = 2500
	cost = 250
	category = Aero
	subcategory = 0
	title = #autoLOC_500115 //#autoLOC_500115 = XM-G50 Radial Air Intake
	manufacturer = #autoLOC_501625 //#autoLOC_501625 = Vac-Co Advanced Suction Systems
	description = #autoLOC_500116 //#autoLOC_500116 = An intake duct version that can be mounted at the sides of a fuselage. Warranty does not cover engine flame-outs or any objects, inanimate or otherwise, sucked in by the intake. Optimized for subsonic flight.
	attachRules = 0,1,0,0,0
	mass = 0.02
	thermalMassModifier = 6.0
	// heatConductivity = 0.06 // half default
	dragModelType = default
	maximum_drag = 0.2
	minimum_drag = 0.2
	angularDrag = 1
	crashTolerance = 10
	breakingForce = 200
	breakingTorque = 200
	maxTemp = 2000
	bulkheadProfiles = srf
	tags = #autoLOC_500117 //#autoLOC_500117 = aero aircraft breathe fligh inlet jet oxygen plane subsonic suck
	MODULE
	{
		name = ModuleResourceIntake
		resourceName = IntakeAir
		checkForOxygen = true
		area = 0.0031
		intakeSpeed = 15
		intakeTransformName = Intake
		machCurve
		{
			key = 1 1 0 0
			key = 1.5 0.9 -0.4312553 -0.4312553
			key = 2.5 0.45 -0.5275364 -0.5275364
			key = 3.5 0.1 0 0
		}
	}
	RESOURCE
	{
		name = IntakeAir
		amount = 2
		maxAmount = 2
	}
	MODULE
	{
		name = ModuleCargoPart
		packedVolume = 2250
	}
}