FIELD: vertical take-off and landing aeroplanes. SUBSTANCE: at least two additional jet engines are located near center of mass of air aircraft on side of fuselage. Engines are mounted vertically or at angle relative to each other in plane perpendicular to aircraft axis. Engines are provided with dampers for reduction of drag. Aircraft wings are tiltable relative to their axes. EFFECT: enhanced maneuverability of aircraft due to installation of additional engines. 2 cl, 3 dwg
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