FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering. Supersonic aircraft comprises fuselage, double sweep swept wing with rear edge high-lift system, power plant consisting of engines, which are spaced along fuselage ends. Front engine is located under crew cabin and equipped with central air intake. Rear engine with air intake is arranged on fuselage aft portion upper surface.
EFFECT: higher safety in case of one of engines failure.
4 cl, 5 dwg
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