FIELD: aircraft engineering.
SUBSTANCE: invention relates to unmanned aerial vehicles. Unmanned aerial vehicle comprises swept-back wing (1), made under condition of using "flying wing" aerodynamic configuration, power plant, including engine with propeller, as well as control elements. Wing (1) in fore end is equipped with power plant and control elements, made in form of foreplane (5) and canard fin (6). Power plant, foreplane (5) and canard fin (6) are located on support (2) above wing upper surface, wherein enabled possibility of wing upper surface and control elements blowing by propeller.
EFFECT: invention increases aircraft lift and maneuverability.
3 cl, 2 dwg
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