Difference between revisions of "Parts/Aero/wings/structural1.cfg"
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< Parts
m (*update to 1.0.1;) |
m (Update config) |
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(One intermediate revision by one other user not shown) | |||
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author = Porkjet | author = Porkjet | ||
rescaleFactor = 1 | rescaleFactor = 1 | ||
− | node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, | + | node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1 |
− | TechRequired = | + | CoMOffset = -0.7, -0.6, 0 |
+ | CoLOffset = -0.7, -0.6, 0 | ||
+ | CoPOffset = -0.7, -0.6, 0 | ||
+ | TechRequired = supersonicFlight | ||
entryCost = 6400 | entryCost = 6400 | ||
cost = 500 | cost = 500 | ||
category = Aero | category = Aero | ||
subcategory = 0 | subcategory = 0 | ||
− | title = Structural Wing Type A | + | title = #autoLOC_500268 //#autoLOC_500268 = Structural Wing Type A |
− | manufacturer = C7 Aerospace Division | + | manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division |
− | description = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings. | + | description = #autoLOC_500269 //#autoLOC_500269 = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings. |
attachRules = 0,1,0,1,1 | attachRules = 0,1,0,1,1 | ||
mass = 0.1 | mass = 0.1 | ||
− | thermalMassModifier = | + | thermalMassModifier = 8.0 // the dang things are light, so 3200 kJ/tonne-K |
// heatConductivity = 0.06 // half default | // heatConductivity = 0.06 // half default | ||
emissiveConstant = 0.95 | emissiveConstant = 0.95 | ||
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angularDrag = 2 | angularDrag = 2 | ||
crashTolerance = 15 | crashTolerance = 15 | ||
− | maxTemp = | + | maxTemp = 2400 // = 3400 |
explosionPotential = 0.1 | explosionPotential = 0.1 | ||
fuelCrossFeed = True | fuelCrossFeed = True | ||
bulkheadProfiles = srf | bulkheadProfiles = srf | ||
+ | tags = #autoLOC_500270 //#autoLOC_500270 = aero aircraft fligh foil lift plane swept | ||
MODEL | MODEL | ||
{ | { | ||
Line 39: | Line 43: | ||
dragAtMaxAoA = 0.3 | dragAtMaxAoA = 0.3 | ||
dragAtMinAoA = 0.0 | dragAtMinAoA = 0.0 | ||
+ | } | ||
+ | MODULE | ||
+ | { | ||
+ | name = ModuleCargoPart | ||
+ | packedVolume = -1 | ||
} | } | ||
} | } | ||
− | |||
}} | }} |
Latest revision as of 11:00, 13 October 2024
PART { name = structuralWing module = Part author = Porkjet rescaleFactor = 1 node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1 CoMOffset = -0.7, -0.6, 0 CoLOffset = -0.7, -0.6, 0 CoPOffset = -0.7, -0.6, 0 TechRequired = supersonicFlight entryCost = 6400 cost = 500 category = Aero subcategory = 0 title = #autoLOC_500268 //#autoLOC_500268 = Structural Wing Type A manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division description = #autoLOC_500269 //#autoLOC_500269 = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings. attachRules = 0,1,0,1,1 mass = 0.1 thermalMassModifier = 8.0 // the dang things are light, so 3200 kJ/tonne-K // 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_500270 //#autoLOC_500270 = aero aircraft fligh foil lift plane swept MODEL { model = Squad/Parts/Aero/wings/structural1 } MODULE { name = ModuleLiftingSurface useInternalDragModel = True deflectionLiftCoeff = 1 dragAtMaxAoA = 0.3 dragAtMinAoA = 0.0 } MODULE { name = ModuleCargoPart packedVolume = -1 } }