FIELD: aeronautical engineering; designing of hypersonic vehicles of various purpose, for example passenger and aero-space planes. SUBSTANCE: flying vehicle includes gas-turbine engines, detonation pulse-jet engines and air intake including subsonic diffusers. Detonation pulse-jet engine module is connected via switch gear to air duct of gas-turbine engine by means of pipe line and to separate air intake which is connected with lower surface of flying vehicle. Air duct is provided with gate for is communication with atmosphere or with subsonic diffuser. Tail section is formed by detonation pulse-jet engine module located linearly along wing span. Detonation pulse-jet engine module may be mounted for turn in vertical plane. EFFECT: reduction of drag and specific consumption of fuel due to extended range of operation of detonation pulse-jet engines. 2 cl, 6 dwg
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