Difference between revisions of "Parts/Aero/airplaneFins/standardCanard.cfg"
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m (BobBot moved page Parts/Aero/standardCanard/standardCanard.cfg to Parts/Aero/airplaneFins/standardCanard.cfg without leaving a redirect: Renamed part configuration file after update.) |
m (Update config) |
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{{Part config|Standard Canard|2=PART | {{Part config|Standard Canard|2=PART | ||
{ | { | ||
− | + | name = CanardController | |
− | + | module = Part | |
− | + | author = C. Jenkins, Porkjet | |
− | + | rescaleFactor = 1 | |
− | + | node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 | |
− | + | CoMOffset = -0.55, -0.15, 0 | |
− | + | CoLOffset = -0.55, -0.15, 0 | |
− | + | CoPOffset = -0.55, -0.15, 0 | |
− | + | TechRequired = advAerodynamics | |
− | + | entryCost = 11400 | |
− | + | cost = 720 | |
− | + | category = Aero | |
− | + | subcategory = 0 | |
− | + | title = #autoLOC_500130 //#autoLOC_500130 = Standard Canard | |
− | + | manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division | |
− | + | description = #autoLOC_500131 //#autoLOC_500131 = Our engineers had a stroke of inspiration after "visiting" the Kerlington production facilities. Introducing our new controllable canards. Warning, hard maneuvering may cause unintended stage separation. | |
− | + | attachRules = 0,1,0,1,0 | |
− | + | mass = 0.1 | |
− | + | thermalMassModifier = 8.0 | |
− | + | // heatConductivity = 0.06 // half default | |
− | + | emissiveConstant = 0.95 | |
− | + | dragModelType = none | |
− | TechRequired = | + | maximum_drag = 0.02 |
− | entryCost = 11400 | + | minimum_drag = 0.02 |
− | cost = 720 | + | angularDrag = 3 |
− | category = Aero | + | crashTolerance = 12 |
− | subcategory = 0 | + | maxTemp = 2400 |
− | title = Standard Canard | + | explosionPotential = 0.1 |
− | manufacturer = C7 Aerospace Division | + | fuelCrossFeed = True |
− | description = Our engineers had a stroke of inspiration after "visiting" the Kerlington production facilities. Introducing our new controllable canards. Warning, hard maneuvering may cause unintended stage separation. | + | bulkheadProfiles = srf |
− | + | tags = #autoLOC_500132 //#autoLOC_500132 = aero (air control (elev fligh (fore lift plane )rudder stab swept tail | |
− | attachRules = 0,1,0,1,0 | + | MODEL |
− | + | { | |
− | + | model = Squad/Parts/Aero/airplaneFins/Canard | |
− | + | } | |
− | + | MODULE | |
− | + | { | |
− | + | name = ModuleControlSurface | |
− | // | + | useInternalDragModel = True |
− | + | dragCoeff = 0.5 | |
− | dragModelType = | + | deflectionLiftCoeff = 0.52 //1.83m^2 |
− | maximum_drag = 0.02 | + | ctrlSurfaceRange = 15 |
− | minimum_drag = 0.02 | + | ctrlSurfaceArea = 1 |
− | angularDrag = 3 | + | actuatorSpeed = 30 |
− | crashTolerance = 12 | + | transformName = ctrlSrf |
− | maxTemp = | + | } |
− | explosionPotential = 0.1 | + | MODULE |
− | fuelCrossFeed = True | + | { |
− | + | name = ModuleCargoPart | |
− | MODULE | + | packedVolume = -1 |
− | { | + | } |
− | |||
− | |||
− | |||
− | |||
− | |||
} | } | ||
− | |||
− | |||
− | |||
− | |||
− | |||
}} | }} |
Latest revision as of 10:59, 13 October 2024
PART { name = CanardController module = Part author = C. Jenkins, Porkjet rescaleFactor = 1 node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 CoMOffset = -0.55, -0.15, 0 CoLOffset = -0.55, -0.15, 0 CoPOffset = -0.55, -0.15, 0 TechRequired = advAerodynamics entryCost = 11400 cost = 720 category = Aero subcategory = 0 title = #autoLOC_500130 //#autoLOC_500130 = Standard Canard manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division description = #autoLOC_500131 //#autoLOC_500131 = Our engineers had a stroke of inspiration after "visiting" the Kerlington production facilities. Introducing our new controllable canards. Warning, hard maneuvering may cause unintended stage separation. attachRules = 0,1,0,1,0 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 = 3 crashTolerance = 12 maxTemp = 2400 explosionPotential = 0.1 fuelCrossFeed = True bulkheadProfiles = srf tags = #autoLOC_500132 //#autoLOC_500132 = aero (air control (elev fligh (fore lift plane )rudder stab swept tail MODEL { model = Squad/Parts/Aero/airplaneFins/Canard } MODULE { name = ModuleControlSurface useInternalDragModel = True dragCoeff = 0.5 deflectionLiftCoeff = 0.52 //1.83m^2 ctrlSurfaceRange = 15 ctrlSurfaceArea = 1 actuatorSpeed = 30 transformName = ctrlSrf } MODULE { name = ModuleCargoPart packedVolume = -1 } }