Difference between revisions of "Parts/Aero/airplaneFins/advancedCanard.cfg"
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Greenjinjo (talk | contribs) (Created page with "<pre> // this is a sample config file, for determining a good file format for defining part parameters // comment line - ignored by cfg parser // empty lines, or lines without...") |
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− | + | {{Part config|Advanced Canard|2=PART | |
− | + | { | |
− | + | name = AdvancedCanard | |
− | + | module = Part | |
− | + | author = C. Jenkins, Porkjet | |
− | + | rescaleFactor = 1 | |
− | // | + | node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 |
− | + | CoLOffset = -0.4, -0.05, 0 | |
− | // | + | CoPOffset = -0.4, -0.05, 0 |
− | // | + | TechRequired = hypersonicFlight |
+ | entryCost = 9200 | ||
+ | cost = 800 | ||
+ | category = Aero | ||
+ | subcategory = 0 | ||
+ | title = Advanced Canard | ||
+ | manufacturer = C7 Aerospace Division | ||
+ | description = Our engineers thought this design looked "high tech" and therefore must be clear improvement on earlier models. | ||
+ | attachRules = 0,1,0,1,0 | ||
+ | mass = 0.08 | ||
+ | thermalMassModifier = 8.0 | ||
+ | // heatConductivity = 0.06 // half default | ||
+ | emissiveConstant = 0.95 | ||
+ | dragModelType = none | ||
+ | maximum_drag = 0.02 | ||
+ | minimum_drag = 0.02 | ||
+ | angularDrag = 3 | ||
+ | crashTolerance = 12 | ||
+ | maxTemp = 2400 | ||
+ | explosionPotential = 0.1 | ||
+ | fuelCrossFeed = True | ||
+ | bulkheadProfiles = srf | ||
+ | MODEL | ||
+ | { | ||
+ | model = Squad/Parts/Aero/airplaneFins/AdvCanard | ||
+ | } | ||
+ | MODULE | ||
+ | { | ||
+ | name = ModuleControlSurface | ||
+ | useInternalDragModel = True | ||
+ | dragCoeff = 0.5 | ||
+ | deflectionLiftCoeff = 0.4 // ~1,4m^2 | ||
+ | ctrlSurfaceRange = 15 | ||
+ | ctrlSurfaceArea = 1 | ||
+ | actuatorSpeed = 30 | ||
+ | transformName = ctrlSrf | ||
+ | } | ||
+ | } | ||
− | + | }} | |
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Latest revision as of 12:09, 27 June 2015
PART { name = AdvancedCanard module = Part author = C. Jenkins, Porkjet rescaleFactor = 1 node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 CoLOffset = -0.4, -0.05, 0 CoPOffset = -0.4, -0.05, 0 TechRequired = hypersonicFlight entryCost = 9200 cost = 800 category = Aero subcategory = 0 title = Advanced Canard manufacturer = C7 Aerospace Division description = Our engineers thought this design looked "high tech" and therefore must be clear improvement on earlier models. attachRules = 0,1,0,1,0 mass = 0.08 thermalMassModifier = 8.0 // heatConductivity = 0.06 // half default emissiveConstant = 0.95 dragModelType = none maximum_drag = 0.02 minimum_drag = 0.02 angularDrag = 3 crashTolerance = 12 maxTemp = 2400 explosionPotential = 0.1 fuelCrossFeed = True bulkheadProfiles = srf MODEL { model = Squad/Parts/Aero/airplaneFins/AdvCanard } MODULE { name = ModuleControlSurface useInternalDragModel = True dragCoeff = 0.5 deflectionLiftCoeff = 0.4 // ~1,4m^2 ctrlSurfaceRange = 15 ctrlSurfaceArea = 1 actuatorSpeed = 30 transformName = ctrlSrf } }