COMBINATION RAMJET-ROCKET ENGINE Russian patent published in 1994 - IPC

Abstract RU 2015390 C1

FIELD: rocket engineering. SUBSTANCE: combination ramjet-rocket engine has sustainer engine and combustion chamber of ramjet engine communicating with air intake. Launching engine is located in combustion chamber in two ring belts with units of radial fixing. One of ring belts is fitted with units of axial fixing. EFFECT: expanded range of application of engine, provision for shockless removal of launching engine from rests. 4 dwg

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RU 2 015 390 C1

Authors

Alekseev N.V.

Dates

1994-06-30—Published

1992-09-01—Filed