ROCKET RAMJET ENGINE Russian patent published in 2002 - IPC

Abstract RU 2195566 C2

FIELD: rocketry. SUBSTANCE: rocket ramjet engine has afterburning chamber with de Laval nozzle, gas generator, solid propellant charge, igniter and air intake. Rotary gas generator is arranged inside afterburning chamber and is provided with half-loop nozzles arranged at angle of 20-30^° relative to engine axis. Invention increases coefficient of fuel afterburning and prevents flame outs. EFFECT: reduced overall dimensions of afterburning chamber and mass of engine as a whole. 2 dwg

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RU 2 195 566 C2

Authors

Lazovik I.N.

Morozov S.A.

Podkopaev A.V.

Dates

2002-12-27—Published

2000-02-21—Filed