FAST ACTING VALVE FOR FEEDING LIQUID, E. G., FUEL COMPONENTS IN LIQUID ROCKET ENGINES
A fast acting valve for feeding liquid, for example fuel components in liquid rocket engines, having a body, membrane, overlapping passing section and membrane piercing organ with pyro drive is described. The pyro drive is not connected in power scheme with the body and is separated from the flow th...
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creator | Belyaev,Yu. V Denisova,A. D Tyurin,Yu. S Ryzhkin,A. S |
description | A fast acting valve for feeding liquid, for example fuel components in liquid rocket engines, having a body, membrane, overlapping passing section and membrane piercing organ with pyro drive is described. The pyro drive is not connected in power scheme with the body and is separated from the flow through section by a flexible diaphragm, controlling the piercing organ and isolating the body from high pressure gases. (Author)
Unedited rough draft trans. of Russian Patent 164 512, pub. 10 Nov 63, appl. no. 864737/24-6. |
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Unedited rough draft trans. of Russian Patent 164 512, pub. 10 Nov 63, appl. no. 864737/24-6.</description><language>eng</language><subject>DIAPHRAGMS(MECHANICS) ; LIQUID ROCKET FUELS ; MEMBRANES ; USSR ; VALVES</subject><creationdate>1965</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0620791$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Belyaev,Yu. V</creatorcontrib><creatorcontrib>Denisova,A. D</creatorcontrib><creatorcontrib>Tyurin,Yu. S</creatorcontrib><creatorcontrib>Ryzhkin,A. S</creatorcontrib><creatorcontrib>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</creatorcontrib><title>FAST ACTING VALVE FOR FEEDING LIQUID, E. G., FUEL COMPONENTS IN LIQUID ROCKET ENGINES</title><description>A fast acting valve for feeding liquid, for example fuel components in liquid rocket engines, having a body, membrane, overlapping passing section and membrane piercing organ with pyro drive is described. The pyro drive is not connected in power scheme with the body and is separated from the flow through section by a flexible diaphragm, controlling the piercing organ and isolating the body from high pressure gases. (Author)
Unedited rough draft trans. of Russian Patent 164 512, pub. 10 Nov 63, appl. no. 864737/24-6.</description><subject>DIAPHRAGMS(MECHANICS)</subject><subject>LIQUID ROCKET FUELS</subject><subject>MEMBRANES</subject><subject>USSR</subject><subject>VALVES</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1965</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZAh1cwwOUXB0DvH0c1cIc_QJc1Vw8w9ScHN1dQGJ-HgGhnq66Ci46im46-kouIW6-ig4-_sG-Pu5-oUEK3j6QVUoBPk7e7uGKLj6uXv6uQbzMLCmJeYUp_JCaW4GGTfXEGcP3ZSSzOT44pLMvNSSeEcXAzMjA3NLQ2MC0gAIHyyN</recordid><startdate>19650824</startdate><enddate>19650824</enddate><creator>Belyaev,Yu. V</creator><creator>Denisova,A. D</creator><creator>Tyurin,Yu. S</creator><creator>Ryzhkin,A. S</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19650824</creationdate><title>FAST ACTING VALVE FOR FEEDING LIQUID, E. G., FUEL COMPONENTS IN LIQUID ROCKET ENGINES</title><author>Belyaev,Yu. V ; Denisova,A. D ; Tyurin,Yu. S ; Ryzhkin,A. S</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06207913</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1965</creationdate><topic>DIAPHRAGMS(MECHANICS)</topic><topic>LIQUID ROCKET FUELS</topic><topic>MEMBRANES</topic><topic>USSR</topic><topic>VALVES</topic><toplevel>online_resources</toplevel><creatorcontrib>Belyaev,Yu. V</creatorcontrib><creatorcontrib>Denisova,A. D</creatorcontrib><creatorcontrib>Tyurin,Yu. S</creatorcontrib><creatorcontrib>Ryzhkin,A. S</creatorcontrib><creatorcontrib>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Belyaev,Yu. V</au><au>Denisova,A. D</au><au>Tyurin,Yu. S</au><au>Ryzhkin,A. S</au><aucorp>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>FAST ACTING VALVE FOR FEEDING LIQUID, E. G., FUEL COMPONENTS IN LIQUID ROCKET ENGINES</btitle><date>1965-08-24</date><risdate>1965</risdate><abstract>A fast acting valve for feeding liquid, for example fuel components in liquid rocket engines, having a body, membrane, overlapping passing section and membrane piercing organ with pyro drive is described. The pyro drive is not connected in power scheme with the body and is separated from the flow through section by a flexible diaphragm, controlling the piercing organ and isolating the body from high pressure gases. (Author)
Unedited rough draft trans. of Russian Patent 164 512, pub. 10 Nov 63, appl. no. 864737/24-6.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | DIAPHRAGMS(MECHANICS) LIQUID ROCKET FUELS MEMBRANES USSR VALVES |
title | FAST ACTING VALVE FOR FEEDING LIQUID, E. G., FUEL COMPONENTS IN LIQUID ROCKET ENGINES |
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