Our technology is based on employing an innovative lift-generating mechanism comprising a number of  ducted compound low angle-of-attack Propellers to lift the aircraft. The compact design of the lift-generating mechanism enables positioning it in the central part of the aircraft’s fuselage, which will enable designing the aircraft’s powertrain with less moving parts, when compared to a conventional Helicopter’s powertrain, making it cheaper to produce and maintain, and less prone to accidents due to component failure. This will also enable operating the aircraft at relatively higher speeds and altitudes, while avoiding the adverse effect of any surrounding wind that maybe encountered during the flight.