AIR VEHICLE

TAIL SITTER STOP-FOLD AIRCRAFT

CANARD ROOT POSITIONED AT THE NOSE TIP AND BEYOND THE NOSE TIP OF AIRCRAFT AND SPACECRAFT RELATED VEHICLES OR PROPELLED/PROJECTILE OBJECTS TO REDUCE DRAG

Aircraft having an AFT engine

Hybrid propulsion vertical take-off and landing aircraft

Unmanned supply delivery aircraft

Canard-locked oblique wing aircraft

Aircraft lifting surface with variable sweep distribution along the span

Energy absorbing impact band

Aircraft spiraling mechanism with jet assistance - E

Aircraft spiraling mechanism with jet assistance—B

Methods for making composite material components especially useful for aircraft, and composite material components thereof

Energy absorbing impact band and method

Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance

Aircraft spiraling mechanism with jet assistance - A

Cover for an aircraft structure

Canard position and dihedral for boom reduction and pitch/directional control

Method and apparatus for rotatably supporting movable components, including canards

Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance

Aircraft spiralling mechanism—c

Aircraft thickness/camber control device for low sonic boom

Canard position and dihedral for boom reduction and pitch/directional control

Apparatus and methods for launching a payload