FIELD: aviation.
SUBSTANCE: unmanned aircraft comprises bearing housing, wing with aerodynamic control elements, power plant including engine, air intake and nozzle, chassis and onboard radar station. Bearing body is made in the form of compartment of small elongation wing with sweep angle of 50...75° along front edge, rear edge of which is made with fracture. Part of rear edge with span, in 2...4 times exceeding width of nozzle located along aircraft axis, has sweep -5...-15°, and outer part is joined with rear edge of wing console and is made with sweep angle -65...-85°, lateral sections are articulated with wing brackets, which is made with elongation of 15...25 and sweep angle of 5...17° along front edge.
EFFECT: invention is aimed at providing a low level of tell-tale features while maintaining high level of aerodynamic efficiency, weight return and controllability.
6 cl, 6 dwg
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