FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used in control over space rocker insertion. Proposed device comprises control and navigation system, gas jet nozzles, gasification system with self-contained gas generator with membrane-type fuel components feed system, acoustic oscillation exciters and gasification product feed mains. The latter are connected via controlled gates with system for fuel feed to appropriate gas generators.
EFFECT: decreased weight of active onboard system of used stage descent.
2 dwg
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