A system and method to control flight of an aircraft. The aircraft having an engine with a rotatably nozzle assembly configured to create forward propulsion and yaw control of the aircraft. The engine exhaust passing through the nozzle is redirected with a valve disposed within the nozzle. Lift is created with a lift system carried by the wing of the aircraft. Additional lift is created during flight with a retractable wing extension disposed within the fixed wing of the aircraft.
AIRCRAFT WING EXTENSION AND NOZZLE SYSTEM
RALLONGE D'AILE D'AERONEF ET SYSTEME DE TUYERES
2015-03-31
Patent
Elektronische Ressource
Englisch