FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular, to light tactical planes with low radio location visibility. The light tactical plane comprises a fuselage with side tail beams, wing consoles, a tail fin, an air intake, a power unit, and a jet nozzle. The lateral tail beams are developed and end with parts rotary on the horizontal axis. Rotary leading edges and internal and external elevons are located on the consoles of the wings with a large sweep. The tail fin is made V-shaped, the consoles whereof are all-moving, serving as both horizontal and vertical tail. The air intake is located in the lower part of the fuselage and partially envelops it from the lower side.
EFFECT: increase in the stability and controllability of the aircraft without deterioration of the characteristics of radio location visibility.
6 cl, 3 dwg
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Authors
Dates
2022-03-23—Published
2021-07-19—Filed