Parts/Aero/wingletAV-T1/wingletAV-T1.cfg
From Kerbal Space Program Wiki
PART { // 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 a '=' sign are also ignored // all other lines are split at the '=' sign, and the left operand is used to know what parameter we are setting // diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs) // each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though) // each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored. // conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value // This is done automatically, so any public variable defined in the loaded module can be accessed this way (provided it's value can be parsed) // --- general parameters --- name = winglet module = Winglet author = HarvesteR // --- asset parameters --- mesh = model.mu scale = 0.1 // --- editor parameters --- TechRequired = stability entryCost = 1500 cost = 500 category = Aero subcategory = 0 title = AV-T1 Winglet // manufacturer = Kerlington Model Rockets and Paper Products Inc description = // attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision attachRules = 0,1,0,0,1 // --- node definitions --- // definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z node_attach = 5.10736, -0.589634, 0.0, 1.0, 0.0, 0.0 // --- standard part parameters --- mass = 0.05 dragModelType = override maximum_drag = 0.02 minimum_drag = 0.02 angularDrag = 5 crashTolerance = 12 maxTemp = 3400 explosionPotential = 0.1 mirrorRefAxis = 0, 0, -1 // --- winglet parameters --- // dragCoeff will override the maximum_drag value dragCoeff = 0.5 deflectionLiftCoeff = 0.3 // --- tweakables (coming soon...) --- // ----- DO NOT EDIT BELOW THIS POINT ------ }