FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Manoeuvrable aircraft contains fuselage, wing, two turbojet engines and gas-dynamic control system which contains gas passage with one pair of nozzles for creation of gas streams in one plane and another pair of nozzles for creation of gas streams in another transversal plane, rotary drive installed on aft body to rotate central gas passage relative to longitudinal axis of fuselage. Fuselage aft portion forms intermediate gas passage with ring base where central gas passage is installed being possible to rotate. Each turbojet engine has gas passage between turbine and nozzle. Gas passages of turbojet engines are provided with corresponding flaps placed symmetrical relative to longitudinal axis of fuselage with possibility to bleed part of gas after corresponding turbine through intermediate gas passage of gas-dynamic control system.
EFFECT: solving the problem of weight saving and flight range increasing while keeping manoeuvrability.
6 cl, 9 dwg
