@PART[straightslat]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.351
		MidChordSweep = 0
		maxdeflect = 45
		b_2 = 1.828
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = straight
	}
}

@PART[spoilerflap]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.478
		MidChordSweep = 0
		maxdeflect = 45
		b_2 = 3.53
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = surface
	}
}

@PART[kruegerflap]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.326
		MidChordSweep = 0
		maxdeflect = 30
		b_2 = 1.66
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = flap
	}
}

@PART[doublefowlerflap]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.9
		MidChordSweep = 0
		maxdeflect = 30
		b_2 = 3.51
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = slata
	}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.47
		MidChordSweep = 0
		maxdeflect = 30
		b_2 = 3.51
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = slatb
	}
}

@PART[migwing]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 1.706
		MidChordSweep = 50
		maxdeflect = 25
		b_2 = 2.08
		TaperRatio = 0.196
		ctrlSurfFrac = 0.155
        transformName = obj_ctrlSrf
	}
}

@PART[warhawkfin]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 2.19
		MidChordSweep = 30
		maxdeflect = 20
		b_2 = 2.45
		TaperRatio = 0.43
		ctrlSurfFrac = 0.465
        transformName = ctrlSrf
	}
}

@PART[wing4]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1.06
		MidChordSweep = 14
		b_2 = 1.9
		TaperRatio = 0.64
		nonSideAttach = 0
	}
}

@PART[wingtip]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.9
		MidChordSweep = -15
		b_2 = 0.51
		TaperRatio = 0.15
		nonSideAttach = 0
	}
}

@PART[hanglel]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.26
		MidChordSweep = 3.5
		b_2 = 1.89
		TaperRatio = 0.54
		nonSideAttach = 1
	}
}

@PART[hangles]:NEEDS[FerramAerospaceResearch] // redo
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.27
		MidChordSweep = 9
		b_2 = 0.93
		TaperRatio = 0.54
		nonSideAttach = 1
	}
}

@PART[vanglel]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.12
		MidChordSweep = 4.3
		b_2 = 0.94
		TaperRatio = 0.44
		nonSideAttach = 1
	}
}

@PART[vangles]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.10
		MidChordSweep = 4
		b_2 = 0.47
		TaperRatio = 0.59
		nonSideAttach = 1
	}
}


// Wronk's config starts here
//Cockpits
//Mk1 Business Cockpit
@PART[citationcockpit]:AFTER[FerramAerospaceResearch]
{
	@MODULE[GeometryPartModule]
	{
		%forceUseMeshes = True
		%ignoreIfNoRenderer = true
	}
}

//Mk3S1.5 Viewer's Cockpit
@PART[hueycockpit]:AFTER[FerramAerospaceResearch]
{
	@MODULE[GeometryPartModule]
	{
		%forceUseMeshes = True
		%ignoreIfNoRenderer = true
	}
}

//Size 2 Non-Commercial Cockpit
@PART[herculescockpit]:AFTER[FerramAerospaceResearch]
{
	@MODULE[GeometryPartModule]
	{
		%forceUseMeshes = True
		%ignoreIfNoRenderer = true
	}
}

@PART[falconcocpit]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1.45
		MidChordSweep = 80
		b_2 = 0.72
		TaperRatio = 0.25
	}
}

//Misc
//Size 2 Crew Cabin
@PART[size2CrewCabin]:AFTER[FerramAerospaceResearch]
{
	@MODULE[GeometryPartModule]
	{
		%forceUseMeshes = True
		%ignoreIfNoRenderer = true
	}
}


//theonegalen's config starts here
//FAT-T3R Aeroplane Main Wing
@PART[bigwing]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 2.48
		MidChordSweep = -4.16
		b_2 = 11.060831
		TaperRatio = 0.5871914171
	}
}

//FATwings
@PART[fatwing0]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1
		MidChordSweep = 0
		b_2 = 3.5
		TaperRatio = 1
	}
}

@PART[fatwing1]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 3.5
		MidChordSweep = 0
		b_2 = 1
		TaperRatio = 1
	}
}

@PART[fatwing2]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.5
		MidChordSweep = 8
		b_2 = 3.5
		TaperRatio = 1
	}
}

@PART[fatwing3]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1.75
		MidChordSweep = 36.75
		b_2 = 1
		TaperRatio = 0
	}
}

@PART[fatwing4]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 3.5
		MidChordSweep = 0
		b_2 = 0.5
		TaperRatio = 1
	}
}

@PART[fatwing5]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1.75
		MidChordSweep = 40
		b_2 = 0.5
		TaperRatio = 0
	}
}

@PART[fatwing6]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.25
		MidChordSweep = -4.1
		b_2 = 3.5
		TaperRatio = 0
	}
}

//Small APP Wings
@PART[smallwingConnector1]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1.14
		MidChordSweep = 0
		b_2 = 0.96
		TaperRatio = 1
	}
}

@PART[smallwingConnector2]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1.87
		MidChordSweep = 0
		b_2 = 0.67
		TaperRatio = 1
	}
}

@PART[smallwingConnector3]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.67
		MidChordSweep = 0
		b_2 = 1.87
		TaperRatio = 1
	}
}

@PART[smallwingConnector4]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.71
		MidChordSweep = -7
		b_2 = 1.87
		TaperRatio = .48
	}
}

@PART[smallwingConnector5]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.34
		MidChordSweep = 7
		b_2 = 1.87
		TaperRatio = 0
	}
}

@PART[smallwingConnector6]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.935
		MidChordSweep = 38
		b_2 = 0.68
		TaperRatio = 0
	}
}

@PART[smallwingConnectortip]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.935
		MidChordSweep = 36.91
		b_2 = 0.58
		TaperRatio = 0.3568965517
	}
}

//CONTROL SURFACES

//Round-Deluxe Winglet
@PART[roundwinglet]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
	@ctrlSurfaceRange = 0
	@ctrlSurfaceArea = 0
    !MODULE[ModuleControlSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.98
		MidChordSweep = 11.14
		maxdeflect = 20
		b_2 = 1.36
		TaperRatio = 0.661
		ctrlSurfFrac = 0.45
        transformName = obj_ctrlSrf
	}
}

@PART[elevon2b]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
	@ctrlSurfaceRange = 0
	@ctrlSurfaceArea = 0
    !MODULE[ModuleControlSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.75
		MidChordSweep = 0
		maxdeflect = 20
		b_2 = 1.825
        nonSideAttach = 1
		TaperRatio = 0
		ctrlSurfFrac = 1
        transformName = ctrlSrf
	}
}

@PART[hlfSrf]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
	@ctrlSurfaceRange = 0
	@ctrlSurfaceArea = 0
    !MODULE[ModuleControlSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.525
		MidChordSweep = 0
		maxdeflect = 20
		b_2 = 0.9125
        nonSideAttach = 1
		TaperRatio = 0
		ctrlSurfFrac = 1
        transformName = elevon
	}
}