Difference between revisions of "Parts/Aero/cones/noseConeAdapter.cfg"
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(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|NCS Adapter|2=PART | |
− | + | { | |
− | + | name = noseConeAdapter | |
− | + | module = Part | |
− | + | author = C. Jenkins, Porkjet | |
− | + | rescaleFactor = 1 | |
− | + | node_stack_top = 0.0, 1.125, 0.0, 0.0, 1.0, 0.0, 0 | |
− | + | node_stack_bottom01 = 0.0, -0.75, 0.0, 0.0, -1.0, 0.0, 1 | |
− | + | node_attach = 0, 0, -0.313, 0.0, 0.0, 1.0 | |
− | + | CenterOfDisplacement = 0.0, -0.2, 0.0 | |
− | + | TechRequired = aerodynamicSystems | |
− | + | entryCost = 6500 | |
− | + | cost = 320 | |
− | name = noseConeAdapter | + | category = Propulsion |
− | module = | + | subcategory = 0 |
− | author = C. Jenkins | + | title = #autoLOC_500157 //#autoLOC_500157 = NCS Adapter |
− | + | manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division | |
− | + | description = #autoLOC_500158 //#autoLOC_500158 = The base of C7 Aerospace's Nose Cone system (NCS) | |
− | + | attachRules = 1,1,1,1,0 | |
− | + | mass = 0.1 | |
− | + | dragModelType = default | |
− | + | maximum_drag = 0.1 | |
− | + | minimum_drag = 0.1 | |
− | + | angularDrag = 1 | |
− | + | crashTolerance = 10 | |
− | + | maxTemp = 2400 | |
− | + | thermalMassModifier = 6.0 | |
− | + | emissiveConstant = 0.95 | |
− | + | tags = #autoLOC_500159 //#autoLOC_500159 = aero aircraft booster )cap cone drag fligh nose plane rocket stab stream tail | |
− | + | fuelCrossFeed = True | |
− | + | bulkheadProfiles = size0, size1 | |
− | + | MODEL | |
− | + | { | |
− | cost = | + | model = Squad/Parts/Aero/cones/Assets/NCS |
− | category = | + | } |
− | subcategory = 0 | + | RESOURCE |
− | title = NCS Adapter | + | { |
− | manufacturer = C7 Aerospace Division | + | name = LiquidFuel |
− | description = The base of C7 Aerospace's Nose Cone system (NCS) | + | amount = 80 |
− | + | maxAmount = 80 | |
− | + | } | |
− | attachRules = 1, | + | MODULE |
− | + | { | |
− | + | name = ModuleAnimateHeat | |
− | + | ThermalAnim = Cone_Heat | |
− | mass = 0. | + | } |
− | dragModelType = default | + | } |
− | maximum_drag = 0. | + | }} |
− | minimum_drag = 0. | ||
− | angularDrag = 1 | ||
− | crashTolerance = | ||
− | maxTemp = | ||
− | fuelCrossFeed = True | ||
− | |||
− | |||
− | // | ||
− |
Latest revision as of 15:50, 10 October 2024
PART { name = noseConeAdapter module = Part author = C. Jenkins, Porkjet rescaleFactor = 1 node_stack_top = 0.0, 1.125, 0.0, 0.0, 1.0, 0.0, 0 node_stack_bottom01 = 0.0, -0.75, 0.0, 0.0, -1.0, 0.0, 1 node_attach = 0, 0, -0.313, 0.0, 0.0, 1.0 CenterOfDisplacement = 0.0, -0.2, 0.0 TechRequired = aerodynamicSystems entryCost = 6500 cost = 320 category = Propulsion subcategory = 0 title = #autoLOC_500157 //#autoLOC_500157 = NCS Adapter manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division description = #autoLOC_500158 //#autoLOC_500158 = The base of C7 Aerospace's Nose Cone system (NCS) attachRules = 1,1,1,1,0 mass = 0.1 dragModelType = default maximum_drag = 0.1 minimum_drag = 0.1 angularDrag = 1 crashTolerance = 10 maxTemp = 2400 thermalMassModifier = 6.0 emissiveConstant = 0.95 tags = #autoLOC_500159 //#autoLOC_500159 = aero aircraft booster )cap cone drag fligh nose plane rocket stab stream tail fuelCrossFeed = True bulkheadProfiles = size0, size1 MODEL { model = Squad/Parts/Aero/cones/Assets/NCS } RESOURCE { name = LiquidFuel amount = 80 maxAmount = 80 } MODULE { name = ModuleAnimateHeat ThermalAnim = Cone_Heat } }