CONTROL ENGINE UNIT FOR SPACECRAFT AND STATIONS WITH THRUSTERS (VERSIONS) Russian patent published in 2000 - IPC

Abstract RU 2148538 C1

FIELD: space engineering; protection of spacecraft against liquid contaminants. SUBSTANCE: according to invention, each protective device is provided with mechanism for turn and/or axial motion. Mechanism shifts this device to position where it does not close section of rocket engine nozzle. EFFECT: enhanced efficiency of protection against liquid contaminants; avoidance of overheating of thrusters in case of abnormal operation; possibility of changing angle of entrapping contaminants relative to engine axis. 3 cl, 2 dwg

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RU 2 148 538 C1

Authors

Rebrov S.G.

Gerasimov Ju.I.

Drozdov V.I.

Dates

2000-05-10—Published

1999-07-08—Filed