FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering. Supersonic convertible aircraft comprises airframe including foreplane, vertical fins, front triangular gull wing, rear wing with trapezoidal outer wings, boost power jet engine and auxiliary cruise ramjet engines. Front wing and rear wing are arranged in closed structure of longitudinal triplane with possibility of in-flight configuration conversion.
EFFECT: invention is aimed at increasing of flight noiselessness by improving of wings laminar supersonic flow.
6 cl, 3 dwg
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