FIELD: aviation.
SUBSTANCE: invention relates to light drones. Unmanned aerial vehicle comprises a fuselage and located on it swept wing, having high elongation without narrowing and positive angle of V-shape, i.e. inclined upward relative to aircraft horizontal plane. Unmanned aerial vehicle also comprises an all-moving Λ-shaped tail unit, having a positive angle of Λ-shape, i.e. deflected downward relative to aircraft horizontal plane, and is the only steering element of aircraft. Besides, air intake is arranged on fuselage top surface, flush with it, while power plant nozzle is recessed into fuselage.
EFFECT: high efficiency of control in all control channels, low air drag, high range and duration of flight and low radar signature.
1 cl, 2 dwg
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