MassWingedVehicle:

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   Mass of a winged vehicle.
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   Form:
   mDry = MassWingedVehicle( mFuel, d )
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   Inputs
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   mFuel      (1,1) Mass of fuel
   d          (1,1) Data structure
                    .massPayload (1,1) Mass of the payload
                    .fuelStructureRatio (1,1) Mass proportional to fuel mass

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   Outputs
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   mDry       (1,1) Dry mass

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