Parts/Aero/airplaneFins/tailfin.cfg
< Parts
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
}
}