FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to unmanned aerial vehicles. Unmanned aerial vehicle comprises a glider, a centre section, a fuselage, a folding wing and an empennage, having a detachable part, vertical (VE) and horizontal (HE) empennage, deflected and fixed propeller groups (PG) in the form of electric power plants with propellers. At that, the unmanned aerial vehicle contains two deflecting PGs located at the ends of the wing, and eight fixed PGs, located in pairs on own remote beams on the sides of the fuselage parallel to the wing. UAV is equipped with front and main landing gear legs. PG are made with 2-bladed propellers with diameter of 1.7 m. Wing and horizontal empennage have deflecting surfaces in form of differential ailerons on wing, altitude controls on HE.
EFFECT: higher aerodynamic efficiency.
6 cl, 3 dwg
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