ROCKET SOLID FUEL ENGINE Russian patent published in 1995 - IPC

Abstract RU 2026501 C1

FIELD: rocket engineering. SUBSTANCE: in burning out of the solid fuel charge of the previous stage, a sleeve interposed between the previous and next stages moves along the engine axis and interacts with the charge by a surface identical with nozzle unit. The profile of passages of the sleeve is an extension of the profile of passages of the nozzle unit. EFFECT: enhanced efficiency. 4 dwg

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RU 2 026 501 C1

Authors

Bajsiev Khadzhi-Murat Khasanovich

Dates

1995-01-09Published

1991-09-06Filed