FIELD: aeronautical engineering. SUBSTANCE: system includes pylon 40 with longitudinal axis and first and second ends 42 and 44. First end 42 of pylon 40 is rotatably secured to flying vehicle and second end 44 extends outside. Pylon 40 rotates around first end 42 of pylon is plane perpendicular to longitudinal axis of flying vehicle. Thrust creating device 26 is secured on second end 44 of pylon 40 for rotation in plane perpendicular to longitudinal axis of pylon 40. Power supply system 32A, 32B is connected with thrust creating device 26 for supply of power. Actuating system is designed for rotating the propeller mounted in ring. Second actuating system is designed for rotating pylon 40 around first end 42. EFFECT: enhanced maneuverability of flying vehicle. 11 cl, 14 dwg
