Difference between revisions of "Parts/Aero/airplaneFins/tailfin.cfg"
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< Parts
m (*update to 1.0;) |
m (*update to 1.0.4;) |
||
Line 6: | Line 6: | ||
rescaleFactor = 1 | rescaleFactor = 1 | ||
node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0, 1 | node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0, 1 | ||
+ | CoLOffset = 0.75, -0.5, 0 | ||
+ | CoPOffset = 0.75, -0.5, 0 | ||
TechRequired = aviation | TechRequired = aviation | ||
entryCost = 3800 | entryCost = 3800 | ||
Line 16: | Line 18: | ||
attachRules = 0,1,0,1,0 | attachRules = 0,1,0,1,0 | ||
mass = 0.125 | mass = 0.125 | ||
− | thermalMassModifier = | + | thermalMassModifier = 8.0 |
// heatConductivity = 0.06 // half default | // heatConductivity = 0.06 // half default | ||
emissiveConstant = 0.95 | emissiveConstant = 0.95 | ||
Line 24: | Line 26: | ||
angularDrag = 2 | angularDrag = 2 | ||
crashTolerance = 12 | crashTolerance = 12 | ||
− | maxTemp = | + | maxTemp = 2400 |
explosionPotential = 0.1 | explosionPotential = 0.1 | ||
fuelCrossFeed = True | fuelCrossFeed = True |
Revision as of 12:09, 27 June 2015
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 CoLOffset = 0.75, -0.5, 0 CoPOffset = 0.75, -0.5, 0 TechRequired = aviation entryCost = 3800 cost = 600 category = Aero subcategory = 0 title = Tail Fin manufacturer = C7 Aerospace Division 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. 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 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 } }