FIELD: hypersonic flying vehicles, aero-space planes for delivery of payload to working and staging orbits. SUBSTANCE: passage of composite ramjet engine is converter into passage of hypersonic ramjet engine and magnetic hydrodynamic accelerator. Composite ramjet engine is provided with air intake with magnetohydrodynamic device containing ionizers, magnets and electrodes located on relatively perpendicular walls of air intake, turbojet engine being mounted after air intake on retractable pylons. EFFECT: improved power characteristics and enhanced economical efficiency due to successive placing of engines in operation and use of magnetohydrodynamic accelerator. 3 dwg
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Authors
Dates
1997-04-10—Published
1993-12-02—Filed