FIELD: aeronautical engineering manned and unmanned flying vehicles of short take-off and landing. SUBSTANCE: proposed flying vehicle has fuselage, lifting aerodynamic surfaces on front portion of fuselage, ventilation sets mounted under them and provided with deflectors at outlet. Diameter of ventilation sets is equal to span of front lifting aerodynamic surfaces. Fuselage is made in form of lifting wing. Mounted in aft portion of fuselage is all-moving lifting aerodynamic surface with vertical rudders secured on its outer edges. Besides that, flying vehicle is provided with free-wheeling main propeller located above ventilation sets. EFFECT: increased lift. 8 cl, 4 dwg
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