COMPOSITE RAMJET ENGINE Russian patent published in 1997 - IPC

Abstract RU 2076829 C1

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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RU 2 076 829 C1

Authors

Kirilkin V.S.

Leshukov V.S.

Ushakov V.M.

Frajshtadt V.L.

Shejkin E.G.

Dates

1997-04-10Published

1993-12-02Filed