CONTROL ENGINE UNIT FOR SPACECRAFT AND STATIONS WITH THRUSTERS (VERSIONS)
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:...
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creator | DROZDOV V.I REBROV S.G GERASIMOV JU.I |
description | 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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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</description><edition>7</edition><language>eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</subject><creationdate>2000</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20000510&DB=EPODOC&CC=RU&NR=2148538C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20000510&DB=EPODOC&CC=RU&NR=2148538C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DROZDOV V.I</creatorcontrib><creatorcontrib>REBROV S.G</creatorcontrib><creatorcontrib>GERASIMOV JU.I</creatorcontrib><title>CONTROL ENGINE UNIT FOR SPACECRAFT AND STATIONS WITH THRUSTERS (VERSIONS)</title><description>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. 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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</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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subjects | AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
title | CONTROL ENGINE UNIT FOR SPACECRAFT AND STATIONS WITH THRUSTERS (VERSIONS) |
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