Difference between revisions of "Parts/Aero/wings/structural2.cfg"
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{{Part config|Structural Wing Type B|2=PART | {{Part config|Structural Wing Type B|2=PART | ||
{ | { | ||
− | + | name = structuralWing2 | |
− | name = structuralWing2 | + | module = Part |
− | module = Part | + | author = Porkjet |
− | author = Porkjet | + | rescaleFactor = 1 |
− | + | node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 | |
− | MODEL | + | CoMOffset = -1.1, -0.1, 0 |
− | { | + | CoLOffset = -1.1, -0.1, 0 |
− | + | CoPOffset = -1.1, -0.1, 0 | |
+ | TechRequired = aerodynamicSystems | ||
+ | entryCost = 6400 | ||
+ | cost = 500 | ||
+ | category = Aero | ||
+ | subcategory = 0 | ||
+ | title = #autoLOC_500271 //#autoLOC_500271 = Structural Wing Type B | ||
+ | manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division | ||
+ | description = #autoLOC_500272 //#autoLOC_500272 = 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 | ||
+ | tags = #autoLOC_500273 //#autoLOC_500273 = aero aircraft fligh foil lift plane swept | ||
+ | MODEL | ||
+ | { | ||
+ | model = Squad/Parts/Aero/wings/structural2 | ||
+ | } | ||
+ | MODULE | ||
+ | { | ||
+ | name = ModuleLiftingSurface | ||
+ | useInternalDragModel = True | ||
+ | deflectionLiftCoeff = 1 | ||
+ | dragAtMaxAoA = 0.3 | ||
+ | dragAtMinAoA = 0.0 | ||
+ | } | ||
+ | MODULE | ||
+ | { | ||
+ | name = ModuleCargoPart | ||
+ | packedVolume = -1 | ||
+ | } | ||
} | } | ||
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}} | }} |
Latest revision as of 11:01, 13 October 2024
PART { name = structuralWing2 module = Part author = Porkjet rescaleFactor = 1 node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 CoMOffset = -1.1, -0.1, 0 CoLOffset = -1.1, -0.1, 0 CoPOffset = -1.1, -0.1, 0 TechRequired = aerodynamicSystems entryCost = 6400 cost = 500 category = Aero subcategory = 0 title = #autoLOC_500271 //#autoLOC_500271 = Structural Wing Type B manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division description = #autoLOC_500272 //#autoLOC_500272 = 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 tags = #autoLOC_500273 //#autoLOC_500273 = aero aircraft fligh foil lift plane swept MODEL { model = Squad/Parts/Aero/wings/structural2 } MODULE { name = ModuleLiftingSurface useInternalDragModel = True deflectionLiftCoeff = 1 dragAtMaxAoA = 0.3 dragAtMinAoA = 0.0 } MODULE { name = ModuleCargoPart packedVolume = -1 } }