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