FIELD: aviation industry. SUBSTANCE: aircraft has fuselage with wings and engine plants, tail unit with horizontal and vertical control surfaces, landing gear, crew cabin, gas dynamic nozzles for creating vertical component of thrust force; gas passage of engine plant is connected with gas passages in wings, horizontal control surfaces and fin through control gas dynamic dampers. Passages in wings, horizontal control surfaces and fin are connected through control valves with gas ducts containing nozzles in lower portion. Gas passages have horizontal gas dynamic dampers; wing tips are provided with front and rear adjustable nozzles. EFFECT: enhanced functional efficiency due to increased lift force and enhanced maneuverability at low flying speeds; avoidance of icing of aerodynamic surfaces. 4 dwg
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