Parts/Aero/airplaneFins/sweptWing.cfg

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// 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 = sweptWing module = Winglet author = C. Jenkins

// --- asset parameters --- mesh = model.mu scale = 0.1


// --- editor parameters --- cost = 500 category = Aero subcategory = 0 title = Swept Wings manufacturer = C7 Aerospace division description = A prototype swept back wing. Made of light weight composite materials. Guaranteed to generate lift, not guaranteed to ensure crew safety.

// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision attachRules = 0,1,0,1,1

// --- node definitions --- // definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z node_attach = 0.0, 0.0, 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 = 2 crashTolerance = 15 maxTemp = 3400 explosionPotential = 0.1 fuelCrossFeed = True // --- winglet parameters --- // dragCoeff will override the maximum_drag value dragCoeff = 0.6 deflectionLiftCoeff = 1.6


// --- tweakables (coming soon...) ---



// ----- DO NOT EDIT BELOW THIS POINT ------ </pre>