Difference between revisions of "Parts/FuelTank/mk2Adapters/standard.cfg"

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m (*update to 0.24.2;)
m (Update config)
 
(6 intermediate revisions by 2 users not shown)
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{{Part config|Mk2 to size 1 Adapter|2=PART
+
{{Part config|Mk2 to 1.25m Adapter|2=PART
 
{
 
{
// Kerbal Space Program - Part Config
+
name = mk2SpacePlaneAdapter
// Fuselage Fuel Tank
+
module = Part
//
+
author = Porkjet
 
+
rescaleFactor = 1
// --- general parameters ---
+
node_stack_top = 0.0, 0.9375, 0.0, 0.0, 1.0, 0.0
name = mk2SpacePlaneAdapter
+
node_stack_bottom = 0.0, -0.9375, 0.0, 0.0, -1.0, 0.0
module = Part
+
node_attach = 0.0, 0.0, 0.7, 0.0, 0.0, -1.0, 1
author = C. Jenkins
+
TechRequired = supersonicFlight
 
+
entryCost = 14600
// --- asset parameters ---
+
cost = 550
mesh = model.mu
+
category = Propulsion
scale = 1.0
+
subcategory = 0
 
+
title = #autoLOC_500559 //#autoLOC_500559 = Mk2 to 1.25m Adapter
// --- node definitions ---
+
manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
node_stack_top = 0.0, 0.76, 0.0, 0.0, 1.0, 0.0
+
description = #autoLOC_500560 //#autoLOC_500560 = Generic Mk2 to Mk1 adapter.
node_stack_bottom = 0.0, -0.76, 0.0, 0.0, 1.0, 0.0
+
attachRules = 1,1,1,1,0
 
+
mass = 0.29
 
+
dragModelType = default
 
+
maximum_drag = 0.2
// --- editor parameters ---
+
minimum_drag = 0.1
TechRequired = supersonicFlight
+
angularDrag = 2
entryCost = 14600
+
crashTolerance = 50
cost = 550
+
breakingForce = 50
category = Propulsion
+
breakingTorque = 50
subcategory = 0
+
maxTemp = 2500 // = 3000
title = Mk2 to size 1 Adapter
+
emissiveConstant = 0.8
manufacturer = C7 Aerospace Division
+
fuelCrossFeed = True
description = This airframe fuselage features the latest in re-entry survivability. Apparently air gets very hot at high speeds (Who knew?!). To combat this, we attached only the finest in slightly used thermal tiles to the under belly.
+
bulkheadProfiles = size1, srf, mk2
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
tags = #autoLOC_500561 //#autoLOC_500561 = fuel fueltank ?lfo liquid oxidizer propellant rocket tank
attachRules = 1,0,1,1,0,0,1
+
MODEL
 
+
{
// --- standard part parameters ---
+
model = Squad/Parts/FuelTank/mk2Adapters/standard
mass = 0.1
+
}
dragModelType = default
+
MODULE
maximum_drag = 0.2
+
{
minimum_drag = 0.3
+
name = ModuleLiftingSurface
angularDrag = 2
+
useInternalDragModel = False
crashTolerance = 50
+
deflectionLiftCoeff = 0.28
breakingForce = 50
+
dragAtMaxAoA = 0.2
breakingTorque = 50
+
dragAtMinAoA = 0.1
maxTemp = 3000
+
}
fuelCrossFeed = True
+
RESOURCE
 
+
{
RESOURCE
+
name = LiquidFuel
{
+
amount = 180
name = LiquidFuel
+
maxAmount = 180
amount = 80
+
}
maxAmount = 80
+
RESOURCE
}
+
{
 +
name = Oxidizer
 +
amount = 220
 +
maxAmount = 220
 +
}
 +
MODULE
 +
{
 +
name = ModuleCargoPart
 +
stackableQuantity = 1
 +
packedVolume = -1
 +
}
 
}
 
}
 
 
}}
 
}}

Latest revision as of 15:46, 10 October 2024

This is the configuration file for Mk2 to 1.25m Adapter.
PART
{
	name = mk2SpacePlaneAdapter
	module = Part
	author = Porkjet
	rescaleFactor = 1
	node_stack_top = 0.0, 0.9375, 0.0, 0.0, 1.0, 0.0
	node_stack_bottom = 0.0, -0.9375, 0.0, 0.0, -1.0, 0.0
	node_attach = 0.0, 0.0, 0.7, 0.0, 0.0, -1.0, 1
	TechRequired = supersonicFlight
	entryCost = 14600
	cost = 550
	category = Propulsion
	subcategory = 0
	title = #autoLOC_500559 //#autoLOC_500559 = Mk2 to 1.25m Adapter
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500560 //#autoLOC_500560 = Generic Mk2 to Mk1 adapter.
	attachRules = 1,1,1,1,0
	mass = 0.29
	dragModelType = default
	maximum_drag = 0.2
	minimum_drag = 0.1
	angularDrag = 2
	crashTolerance = 50
	breakingForce = 50
	breakingTorque = 50
	maxTemp = 2500 // = 3000
	emissiveConstant = 0.8
	fuelCrossFeed = True
	bulkheadProfiles = size1, srf, mk2
	tags = #autoLOC_500561 //#autoLOC_500561 = fuel fueltank ?lfo liquid oxidizer propellant rocket tank
	MODEL
	{
		model = Squad/Parts/FuelTank/mk2Adapters/standard
	}
	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = False
		deflectionLiftCoeff = 0.28
		dragAtMaxAoA = 0.2
		dragAtMinAoA = 0.1
	}
	RESOURCE
	{
		name = LiquidFuel
		amount = 180
		maxAmount = 180
	}
	RESOURCE
	{
		name = Oxidizer
		amount = 220
		maxAmount = 220
	}
	MODULE
	{
		name = ModuleCargoPart	
		stackableQuantity = 1
		packedVolume = -1
	}	
}