DOUBLE BASE-SYSTEM PROPELLANT COMPOSITION AND PRODUCTION THEREOF
PURPOSE:To obtain the subject composition having high specific impulse and combustion speed and excellent producibility containing aliphatic polyether having terminal hydroxyl group expressed by specific formula and isocyanate compound in raw material in a double base-system propellant having fixed...
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| creator | MACHIDA HIDEKI SHIMIZU HARUAKI SOTANI TOMOHIRO KUBOTA NAMINOSUKE |
| description | PURPOSE:To obtain the subject composition having high specific impulse and combustion speed and excellent producibility containing aliphatic polyether having terminal hydroxyl group expressed by specific formula and isocyanate compound in raw material in a double base-system propellant having fixed component composition. CONSTITUTION:A double base(DB) propellant substantially composed of nitrocellulose(NC) and nitroglycerin(NG) or liquid nitroester as principal components is produced as follows. 3-20wt.% aliphatic polyether expressed by the formula having terminal hydroxyl group containing azide methyl group in side chain and isocyanate compound are further contained in said raw material. Then, said polyether is made to three-dimensionally crosslinked structure to afford the aimed DB-system propellant composition. Besides, said polyether is suitable as a binder of DB propellant having excellent miscibility with NG. |
| format | Patent |
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CONSTITUTION:A double base(DB) propellant substantially composed of nitrocellulose(NC) and nitroglycerin(NG) or liquid nitroester as principal components is produced as follows. 3-20wt.% aliphatic polyether expressed by the formula having terminal hydroxyl group containing azide methyl group in side chain and isocyanate compound are further contained in said raw material. Then, said polyether is made to three-dimensionally crosslinked structure to afford the aimed DB-system propellant composition. Besides, said polyether is suitable as a binder of DB propellant having excellent miscibility with NG.</description><language>eng</language><subject>CHEMISTRY ; EXPLOSIVES ; EXPLOSIVES OR THERMIC COMPOSITIONS ; GAS-ATTACK COMPOSITIONS ; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART) ; MANUFACTURE THEREOF ; MATCHES ; MEANS FOR GENERATING SMOKE OR MIST ; METALLURGY ; USE OF SINGLE SUBSTANCES AS EXPLOSIVES</subject><creationdate>1991</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=19910227&DB=EPODOC&CC=JP&NR=H0345585A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19910227&DB=EPODOC&CC=JP&NR=H0345585A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MACHIDA HIDEKI</creatorcontrib><creatorcontrib>SHIMIZU HARUAKI</creatorcontrib><creatorcontrib>SOTANI TOMOHIRO</creatorcontrib><creatorcontrib>KUBOTA NAMINOSUKE</creatorcontrib><title>DOUBLE BASE-SYSTEM PROPELLANT COMPOSITION AND PRODUCTION THEREOF</title><description>PURPOSE:To obtain the subject composition having high specific impulse and combustion speed and excellent producibility containing aliphatic polyether having terminal hydroxyl group expressed by specific formula and isocyanate compound in raw material in a double base-system propellant having fixed component composition. CONSTITUTION:A double base(DB) propellant substantially composed of nitrocellulose(NC) and nitroglycerin(NG) or liquid nitroester as principal components is produced as follows. 3-20wt.% aliphatic polyether expressed by the formula having terminal hydroxyl group containing azide methyl group in side chain and isocyanate compound are further contained in said raw material. Then, said polyether is made to three-dimensionally crosslinked structure to afford the aimed DB-system propellant composition. Besides, said polyether is suitable as a binder of DB propellant having excellent miscibility with NG.</description><subject>CHEMISTRY</subject><subject>EXPLOSIVES</subject><subject>EXPLOSIVES OR THERMIC COMPOSITIONS</subject><subject>GAS-ATTACK COMPOSITIONS</subject><subject>GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)</subject><subject>MANUFACTURE THEREOF</subject><subject>MATCHES</subject><subject>MEANS FOR GENERATING SMOKE OR MIST</subject><subject>METALLURGY</subject><subject>USE OF SINGLE SUBSTANCES AS EXPLOSIVES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1991</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBw8Q918nFVcHIMdtUNjgwOcfVVCAjyD3D18XH0C1Fw9vcN8A_2DPH091Nw9HMBSbmEOoO5IR6uQa7-bjwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JN4rwMPA2MTU1MLU0ZgIJQCNxSrn</recordid><startdate>19910227</startdate><enddate>19910227</enddate><creator>MACHIDA HIDEKI</creator><creator>SHIMIZU HARUAKI</creator><creator>SOTANI TOMOHIRO</creator><creator>KUBOTA NAMINOSUKE</creator><scope>EVB</scope></search><sort><creationdate>19910227</creationdate><title>DOUBLE BASE-SYSTEM PROPELLANT COMPOSITION AND PRODUCTION THEREOF</title><author>MACHIDA HIDEKI ; SHIMIZU HARUAKI ; SOTANI TOMOHIRO ; KUBOTA NAMINOSUKE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JPH0345585A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1991</creationdate><topic>CHEMISTRY</topic><topic>EXPLOSIVES</topic><topic>EXPLOSIVES OR THERMIC COMPOSITIONS</topic><topic>GAS-ATTACK COMPOSITIONS</topic><topic>GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)</topic><topic>MANUFACTURE THEREOF</topic><topic>MATCHES</topic><topic>MEANS FOR GENERATING SMOKE OR MIST</topic><topic>METALLURGY</topic><topic>USE OF SINGLE SUBSTANCES AS EXPLOSIVES</topic><toplevel>online_resources</toplevel><creatorcontrib>MACHIDA HIDEKI</creatorcontrib><creatorcontrib>SHIMIZU HARUAKI</creatorcontrib><creatorcontrib>SOTANI TOMOHIRO</creatorcontrib><creatorcontrib>KUBOTA NAMINOSUKE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MACHIDA HIDEKI</au><au>SHIMIZU HARUAKI</au><au>SOTANI TOMOHIRO</au><au>KUBOTA NAMINOSUKE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DOUBLE BASE-SYSTEM PROPELLANT COMPOSITION AND PRODUCTION THEREOF</title><date>1991-02-27</date><risdate>1991</risdate><abstract>PURPOSE:To obtain the subject composition having high specific impulse and combustion speed and excellent producibility containing aliphatic polyether having terminal hydroxyl group expressed by specific formula and isocyanate compound in raw material in a double base-system propellant having fixed component composition. CONSTITUTION:A double base(DB) propellant substantially composed of nitrocellulose(NC) and nitroglycerin(NG) or liquid nitroester as principal components is produced as follows. 3-20wt.% aliphatic polyether expressed by the formula having terminal hydroxyl group containing azide methyl group in side chain and isocyanate compound are further contained in said raw material. Then, said polyether is made to three-dimensionally crosslinked structure to afford the aimed DB-system propellant composition. Besides, said polyether is suitable as a binder of DB propellant having excellent miscibility with NG.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | CHEMISTRY EXPLOSIVES EXPLOSIVES OR THERMIC COMPOSITIONS GAS-ATTACK COMPOSITIONS GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART) MANUFACTURE THEREOF MATCHES MEANS FOR GENERATING SMOKE OR MIST METALLURGY USE OF SINGLE SUBSTANCES AS EXPLOSIVES |
| title | DOUBLE BASE-SYSTEM PROPELLANT COMPOSITION AND PRODUCTION THEREOF |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-31T12%3A29%3A50IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=MACHIDA%20HIDEKI&rft.date=1991-02-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJPH0345585A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |