In addition the rear ducted systems may pivot up to less then sixty degrees forward and backwards to deliver the vector thrust where the aircraft needs it to be. The design of a low speed "T-Tail" houses the function of yaw control with multiple rudders located on its vertical stabilizer, and elevators on its horizontal stabilizer. Giving the UV-4 a unique control system and improved maneuverability. The function of the ducted system serves as a mean of channeling pressure and vectoring thrust. Delivering an efficient means of lift using smaller and therefore quieter propeller then traditional helicopters. The system made its launch in 2015, since then advances and improvements have been completed to the airframe and power plant configurations. Created as a means to display the potential of a ducted fan rotorcraft powered by multiple electric motors.
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