FIELD: aviation.
SUBSTANCE: invention relates to combat aircraft complexes (CAC) with unmanned return aircraft (URA). CAC includes more than one unmanned return aircraft (URA), made with possibility of start from both inclined launcher with URA rocket booster, or its mortar launch from vertical transport-launching container (TLC), or drop from aircraft carrier, and after it performs its mission of automatic return and vertical or horizontal landing using parachute-jet system (PJS) or retractable tricycle wheel landing gear. URA has hexahedral fuselage, two swept-forward and swept-back wings. Wing folding consoles are mounted in fuselage aft and fore parts or its central part in front and behind along flight from center of mass, on lower and upper or on upper and lower sides of its hexagonal transverse shape respectively.
EFFECT: decreased overall dimensions in transport and travelling configuration, higher speed, longer range.
2 cl, 3 dwg
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