The aircraft can include: an
airframe, a tilt mechanism, a
payload housing, and can optionally include an
impact attenuator, a set of
ground support members (e.g., struts), a set of power sources, and a set of control elements. The
airframe can include: a set of rotors and a set of support members. By utilizing a larger rotor blade area (and / or larger rotor disc area) and adjusting the
blade pitch and RPM, the rotors can augment the lift generated by the aerodynamic profile of the aircraft in the
forward flight mode in addition to providing forward thrust. Variants generating lift with the rotors can reduce or eliminate additional control surfaces (e.g., wing flaps, ailerons, ruddervators, elevators,
rudder, etc.) on the aircraft since the thrust and
motor torque is controllable (thereby indirectly controlling lift) at each rotor, thereby enabling
pitch,
yaw, and / or roll control during
forward flight.