Difference between revisions of "Parts/Aero/wings/structural2.cfg"
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< Parts
m (*update to 1.0.1;) |
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 = -1.1, -0.1, 0 | ||
+ | CoPOffset = -1.1, -0.1, 0 | ||
TechRequired = aerodynamicSystems | TechRequired = aerodynamicSystems | ||
entryCost = 6400 | entryCost = 6400 | ||
Line 16: | Line 18: | ||
attachRules = 0,1,0,1,1 | attachRules = 0,1,0,1,1 | ||
mass = 0.1 | mass = 0.1 | ||
− | 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 = 15 | crashTolerance = 15 | ||
− | maxTemp = | + | maxTemp = 2400 // = 3400 |
explosionPotential = 0.1 | explosionPotential = 0.1 | ||
fuelCrossFeed = True | fuelCrossFeed = True |
Revision as of 12:10, 27 June 2015
PART { name = structuralWing2 module = Part author = Porkjet rescaleFactor = 1 node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 CoLOffset = -1.1, -0.1, 0 CoPOffset = -1.1, -0.1, 0 TechRequired = aerodynamicSystems entryCost = 6400 cost = 500 category = Aero subcategory = 0 title = Structural Wing Type B manufacturer = C7 Aerospace Division description = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. attachRules = 0,1,0,1,1 mass = 0.1 thermalMassModifier = 8.0 // heatConductivity = 0.06 // half default emissiveConstant = 0.95 dragModelType = none maximum_drag = 0.02 minimum_drag = 0.02 angularDrag = 2 crashTolerance = 15 maxTemp = 2400 // = 3400 explosionPotential = 0.1 fuelCrossFeed = True bulkheadProfiles = srf MODEL { model = Squad/Parts/Aero/wings/structural2 } MODULE { name = ModuleLiftingSurface useInternalDragModel = True deflectionLiftCoeff = 1 dragAtMaxAoA = 0.3 dragAtMinAoA = 0.0 } }