FIELD: aviation.
SUBSTANCE: invention relates to aviation, in particular to supersonic aircraft with a low level of radar visibility. The multifunctional supersonic single-engine aircraft contains a fuselage, a trapezoidal wing, a V-shaped all-moving tail, developed side beams, a lower-side air intake engine located under the nose of the fuselage, the channel of which is located along the axis of symmetry of the aircraft, a central and side cargo compartments, a single-engine power plant, including an engine with a jet rotary nozzle located along the axis of symmetry of the aircraft.
EFFECT: aircraft design and layout scheme provide a reduction in the geometric and weight dimensions of the aircraft, a decrease in aerodynamic drag, a decrease in RCS and radar visibility, high flight performance, maneuverability, high stability and controllability of the aircraft, an increase in the relative volume of cargo compartments, the ability to accommodate bulky cargo for various purposes and versatility.
10 cl, 7 dwg
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Authors
Dates
2022-04-25—Published
2021-07-19—Filed