FIELD: aviation.
SUBSTANCE: drone aircraft contains a fuselage and a wing (1), made according to the aerodynamic configuration "flying wing", the power plant, which is placed on a support (2) over the top surface of the wing (1) in its nose part and can be formed as a motor ( 3), coaxial with propfan (4), or a motor with low noise birotating propfan blades, or as a motor coaxial with the propeller. The controller in the shape of front horizontal (5) and front vertical canards (6) is installed on the support (2) of the power plant. The takeoff and landing supports may be in the form of at least three telescopic pneumatic supports (7), or are made as a three-point wheel landing gear, or in the form of turning controlled hydrofoil, mounted on the fillet fairing at the lower surface of the wing (1).
EFFECT: invention improves maneuverability and flight performance.
12 cl, 5 dwg
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