Difference between revisions of "Parts/Aero/airplaneFins/tailfin.cfg"

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m (BobBot moved page Parts/Aero/tailfin/part.cfg to Parts/Aero/airplaneFins/tailfin.cfg without leaving a redirect: Renamed part configuration file after update.)
m (Update config)
 
(2 intermediate revisions by one other user not shown)
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{{Part config|Tail Fin|2=PART
 
{{Part config|Tail Fin|2=PART
 
{
 
{
−
// this is a sample config file, for determining a good file format for defining part parameters
+
name = tailfin
−
// 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
+
rescaleFactor = 1
−
// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
+
node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0, 1
−
// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
+
CoMOffset = 0.75, -0.5, 0
−
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
CoLOffset = 0.75, -0.5, 0
−
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
CoPOffset = 0.75, -0.5, 0
−
// 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)
+
TechRequired = aviation
−
 
+
entryCost = 3800
−
 
+
cost = 600
−
// --- general parameters ---
+
category = Aero
−
name = tailfin
+
subcategory = 0
−
module = Winglet
+
title = #autoLOC_500136 //#autoLOC_500136 = Tail Fin
−
author = C. Jenkins
+
manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
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+
description = #autoLOC_500137 //#autoLOC_500137 = This tailfin has passed extensive modeling in our patented P.A.S system.(Paper Airplane Simulation). This fin has been blunted to prevent accidental dismemberment of installing technicians.
−
// --- asset parameters ---
+
attachRules = 0,1,0,1,0
−
mesh = model.mu
+
mass = 0.125
−
scale = 0.1
+
thermalMassModifier = 8.0
−
 
+
// heatConductivity = 0.06 // half default
−
 
+
emissiveConstant = 0.95
−
// --- editor parameters ---
+
dragModelType = none
−
TechRequired = aerodynamicSystems
+
maximum_drag = 0.02
−
entryCost = 3800
+
minimum_drag = 0.02
−
cost = 600
+
angularDrag = 2
−
category = Aero
+
crashTolerance = 12
−
subcategory = 0
+
maxTemp = 2400
−
title = Tail Fin
+
explosionPotential = 0.1
−
manufacturer = C7 Aerospace Division
+
fuelCrossFeed = True
−
description = This tailfin has passed extensive modeling in our patented P.A.S system.(Paper Airplane Simulation). This fin has been blunted to prevent accidental dismemberment of installing technicians.
+
bulkheadProfiles = srf
−
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
tags = #autoLOC_500138 //#autoLOC_500138 = aero (air canard control (elev fligh (fore lift plane )rudder stab swept
−
attachRules = 0,1,0,1,1
+
MODEL
−
 
+
{
−
// --- node definitions ---
+
model = Squad/Parts/Aero/airplaneFins/TailFin
−
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
+
}
−
node_attach = 0, 0, 0.0, -1.0, 0.0, 0.0
+
MODULE
−
 
+
{
−
 
+
name = ModuleControlSurface
−
// --- standard part parameters ---
+
useInternalDragModel = True
−
mass = 0.02
+
dragCoeff = 0.6
−
dragModelType = override
+
deflectionLiftCoeff = 0.61 // 2.18m^2
−
maximum_drag = 0.02
+
ctrlSurfaceRange = 25
−
minimum_drag = 0.02
+
ctrlSurfaceArea = 1
−
angularDrag = 2
+
actuatorSpeed = 25
−
crashTolerance = 12
+
transformName = ctrlSrf
−
maxTemp = 3400
+
}
−
explosionPotential = 0.1
+
MODULE
−
fuelCrossFeed = True
+
{
−
 
+
name = ModuleCargoPart
−
// --- winglet parameters ---
+
packedVolume = -1
−
// dragCoeff will override the maximum_drag value
+
}
−
dragCoeff = 0.5
 
−
deflectionLiftCoeff = 0.3
 
−
 
 
−
 
 
−
 
 
−
// --- tweakables (coming soon...) ---
 
−
 
 
−
 
 
−
 
 
−
 
 
−
// ----- DO NOT EDIT BELOW THIS POINT ------
 
−
 
 
 
}
 
}
−
 
 
}}
 
}}

Latest revision as of 11:00, 13 October 2024

This is the configuration file for Tail Fin. 
PART
{
	name = tailfin
	module = Part
	author = C. Jenkins, Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0, 1
	CoMOffset = 0.75, -0.5, 0
	CoLOffset = 0.75, -0.5, 0
	CoPOffset = 0.75, -0.5, 0
	TechRequired = aviation
	entryCost = 3800
	cost = 600
	category = Aero
	subcategory = 0
	title = #autoLOC_500136 //#autoLOC_500136 = Tail Fin
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500137 //#autoLOC_500137 = This tailfin has passed extensive modeling in our patented P.A.S system.(Paper Airplane Simulation). This fin has been blunted to prevent accidental dismemberment of installing technicians.
	attachRules = 0,1,0,1,0
	mass = 0.125
	thermalMassModifier = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 2
	crashTolerance = 12
	maxTemp = 2400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	tags = #autoLOC_500138 //#autoLOC_500138 = aero (air canard control (elev fligh (fore lift plane )rudder stab swept
	MODEL
	{
		model = Squad/Parts/Aero/airplaneFins/TailFin
	}
	MODULE
	{
		name = ModuleControlSurface
		useInternalDragModel = True
		dragCoeff = 0.6
		deflectionLiftCoeff = 0.61		// 2.18m^2
		ctrlSurfaceRange = 25
		ctrlSurfaceArea = 1
		actuatorSpeed = 25
		transformName = ctrlSrf
	}
	MODULE
	{
		name = ModuleCargoPart		
		packedVolume = -1
	}
}
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