FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to highly maneuverable aircraft with jet engines. Method of flying an aircraft with an integrated control system on a difficult-predictable and low-vulnerability trajectory consists in that in maneuvering mode to change the position of the aircraft in space, coordinated emission of the jet from nozzles with CTV, spatial action of vertical reactive moments, as well as axial traction forces on aircraft, which leads to abrupt change of flight trajectory on height, along horizontal and diagonal, in plane across direction of longitudinal flight of aircraft. Jet high maneuverable aircraft includes fuselage, wings with elements of mechanization, control system, power plant of jet engines with outlet nozzles located on perimeter of disk-like fuselage or on lateral arms of fuselage. On lateral sides of fuselage front part jet engines are located with possibility of rotation around vertical axis and change of thrust vector (CTV). Mid-flight engine in the tail part of the fuselage has a central nozzle and one or a group of side nozzles with CTV.
EFFECT: higher maneuverability of high-speed aircraft.
2 cl, 44 dwg
