wing_procedural_typeA.cfg

PART
{
    // --- general parameters ---
    name = B9_Aero_Wing_Procedural_TypeA
    module = Part
    author = bac9

    // --- asset parameters ---
    MODEL
    {
        model = B9_Aerospace_ProceduralWings/Parts/Aero_Wing_Procedural/wing_procedural_typeA
    }
    scale = 1
    rescaleFactor = 0.1

    // --- editor parameters ---
    TechRequired = advAerodynamics
    entryCost = 10000
    cost = 0
    category = Aero
    subcategory = 0
    title = B9-PW Procedural wing
    manufacturer = Tetragon Projects
    description = Procedural wing you can shape in any way you want using the context menu. Press J while pointing at this part to open the editor window allowing you to edit the shape and materials of this part. You can exit the editing mode by switching to editing of another part in the very same way, or by pressing J again, or by closing the window. The window can also be opened and closed using the B9 button in the bottom-right corner of the screen.

    // 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 = none
    crashTolerance = 15
    maxTemp = 2400
    explosionPotential = 0.1
    fuelCrossFeed = True
    breakingTorque = 100
    breakingForce = 100
	
	thermalMassModifier = 4.0
	emissiveConstant = 0.95
	skinInternalConductionMult = 5
	bulkheadProfiles = srf

	MODULE
	{
		name = ModuleLiftingSurface
		useInternalDragModel = True
		deflectionLiftCoeff = 2.0
		dragAtMaxAoA = 0.5
		dragAtMinAoA = 0.0
	}
	
    MODULE
    {
        name = WingProcedural
        isCtrlSrf = False
        isWingAsCtrlSrf = False
    }

    MODULE:NEEDS[modularFuelTanks|RealFuels]
    {
        name = ModuleFuelTanks

        volume = 3.84
        basemass = -1
        utilizationTweakable = true
        utilization = 0.5
        type = Default
        
        //see: https://github.com/search?q=tankVolumeConversion&type=Code
        tankVolumeConversion:NEEDS[modularFuelTanks] = 200
    }
}

@PART[B9_Aero_Wing_Procedural_TypeA]:NEEDS[ferramGraph] 
{
	!MODULE[ModuleLiftingSurface] {}

    MODULE
    {
        name = FARWingAerodynamicModel
        MAC = 4
        MidChordSweep = 0
        b_2 = 4
        TaperRatio = 1
    }
}