FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular, to the design of the aviation unmanned anti-submarine and anti-ship complexes. Flying robot-carrier of missiles (FLCM) comprises fuselage, carrying wing, tail unit, onboard control system providing independent or remote control, onboard power supply, aircraft anti-submarine and / or anti-ship missiles. FLCM is equipped at the ends of the external beams of the tail beams with steering jet nozzles operating in the horizontal plane in turn, changing the heading balancing during operation of the rotor. Latter is equipped with two non-self-winding turbojet two-circuit engines with air bleed from compressors and power to the rotor drive controlled by the nozzle thrust vector for horizontal flight when the shaft of the double-bladed rotor shaft is retracted. Wing blades and wings have asymmetrically variable sweep with angle χ=±26° or χ=±60° opposite sweep and form a system of wings of X-shaped sweep.
EFFECT: higher speed and range of flight, higher probability of destruction of surface or underwater target located at long range.
4 cl, 3 dwg, 1 tbl
