Difference between revisions of "Parts/Aero/wingletAV-T1/wingletAV-T1.cfg"
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(Created page with "{{Part config|AV-T1 Winglet|2=PART { // this is a sample config file, for determining a good file format for defining part parameters // comment line - ignored by cfg parser /...") |
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{{Part config|AV-T1 Winglet|2=PART | {{Part config|AV-T1 Winglet|2=PART | ||
{ | { | ||
− | + | name = winglet | |
− | + | module = Part | |
− | + | author = HarvesteR | |
− | + | mesh = model.mu | |
− | + | scale = 0.1 | |
− | + | TechRequired = stability | |
− | + | entryCost = 1500 | |
− | + | cost = 500 | |
− | + | category = Aero | |
− | + | subcategory = 0 | |
− | + | title = #autoLOC_500223 //#autoLOC_500223 = AV-T1 Winglet | |
− | + | description = #autoLOC_500224 //#autoLOC_500224 = Nothing is really known about this thing. Use it at your own risk. | |
− | name = winglet | + | attachRules = 0,1,0,0,1 |
− | module = | + | node_attach = 5.10736, -0.589634, 0.0, 1.0, 0.0, 0.0 |
− | author = HarvesteR | + | CoMOffset = 0.08, -0.2, 0.00664 |
− | + | CoLOffset = 0.08, -0.2, 0.00664 | |
− | + | CoPOffset = 0.08, -0.2, 0.00664 | |
− | mesh = model.mu | + | mass = 0.037 |
− | scale = 0.1 | + | thermalMassModifier = 8.0 |
− | + | // heatConductivity = 0.06 // half default | |
− | + | emissiveConstant = 0.95 | |
− | + | dragModelType = none | |
− | TechRequired = stability | + | maximum_drag = 0.02 |
− | entryCost = 1500 | + | minimum_drag = 0.02 |
− | cost = 500 | + | angularDrag = 5 |
− | category = Aero | + | crashTolerance = 12 |
− | subcategory = 0 | + | maxTemp = 2400 |
− | title = AV-T1 Winglet | + | explosionPotential = 0.1 |
− | // | + | mirrorRefAxis = 0, 0, -1 |
− | + | bulkheadProfiles = srf | |
− | + | tags = #autoLOC_500225 //#autoLOC_500225 = aero aircraft fin lift plane rocket stab swept | |
− | attachRules = 0,1,0,0,1 | + | MODULE |
− | + | { | |
− | + | name = ModuleLiftingSurface | |
− | + | useInternalDragModel = True | |
− | + | deflectionLiftCoeff = 0.37 | |
− | + | dragAtMaxAoA = 0.3 | |
− | + | } | |
− | // | + | MODULE |
− | + | { | |
− | dragModelType = | + | name = ModuleCargoPart |
− | maximum_drag = 0.02 | + | packedVolume = 400 |
− | minimum_drag = 0.02 | + | } |
− | angularDrag = 5 | ||
− | crashTolerance = 12 | ||
− | maxTemp = | ||
− | explosionPotential = 0.1 | ||
− | |||
− | mirrorRefAxis = 0, 0, -1 | ||
− | |||
− | // | ||
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} | } | ||
}} | }} |
Latest revision as of 11:10, 13 October 2024
PART { name = winglet module = Part author = HarvesteR mesh = model.mu scale = 0.1 TechRequired = stability entryCost = 1500 cost = 500 category = Aero subcategory = 0 title = #autoLOC_500223 //#autoLOC_500223 = AV-T1 Winglet description = #autoLOC_500224 //#autoLOC_500224 = Nothing is really known about this thing. Use it at your own risk. attachRules = 0,1,0,0,1 node_attach = 5.10736, -0.589634, 0.0, 1.0, 0.0, 0.0 CoMOffset = 0.08, -0.2, 0.00664 CoLOffset = 0.08, -0.2, 0.00664 CoPOffset = 0.08, -0.2, 0.00664 mass = 0.037 thermalMassModifier = 8.0 // heatConductivity = 0.06 // half default emissiveConstant = 0.95 dragModelType = none maximum_drag = 0.02 minimum_drag = 0.02 angularDrag = 5 crashTolerance = 12 maxTemp = 2400 explosionPotential = 0.1 mirrorRefAxis = 0, 0, -1 bulkheadProfiles = srf tags = #autoLOC_500225 //#autoLOC_500225 = aero aircraft fin lift plane rocket stab swept MODULE { name = ModuleLiftingSurface useInternalDragModel = True deflectionLiftCoeff = 0.37 dragAtMaxAoA = 0.3 } MODULE { name = ModuleCargoPart packedVolume = 400 } }