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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Authors
Dates
1995-01-09—Published
1991-09-06—Filed