Composite double base propellant with HMX oxidizer
1. A solid propellant composition comprising, by weight, 50 percent cyclotetramethylene tetranitramine, 17.7 percent nitrocellulose, 22.1 percent nitroglycerin, 5.2 percent triacetin, 0.5 percent diethylphthalate, 2.0 percent basic lead beta resorcylate, 2.0 percent basic cupric salicylate, 0.5 perc...
Gespeichert in:
| Hauptverfasser: | , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | LO PRESTI ARTHUR BAUMANN ROBERT P |
| description | 1. A solid propellant composition comprising, by weight, 50 percent cyclotetramethylene tetranitramine, 17.7 percent nitrocellulose, 22.1 percent nitroglycerin, 5.2 percent triacetin, 0.5 percent diethylphthalate, 2.0 percent basic lead beta resorcylate, 2.0 percent basic cupric salicylate, 0.5 percent 2-nitrodiphenylamine, and 0.02 percent carbon black. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US3878003A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US3878003A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US3878003A3</originalsourceid><addsrcrecordid>eNrjZDByzs8tyC_OLElVSMkvTcpJVUhKLE5VKCjKL0jNyUnMK1EozyzJUPDwjVDIr8hMyaxKLeJhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfGhwcYW5hYGBsaOxoRVAAAiRCte</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Composite double base propellant with HMX oxidizer</title><source>esp@cenet</source><creator>LO PRESTI; ARTHUR ; BAUMANN; ROBERT P</creator><creatorcontrib>LO PRESTI; ARTHUR ; BAUMANN; ROBERT P</creatorcontrib><description>1. A solid propellant composition comprising, by weight, 50 percent cyclotetramethylene tetranitramine, 17.7 percent nitrocellulose, 22.1 percent nitroglycerin, 5.2 percent triacetin, 0.5 percent diethylphthalate, 2.0 percent basic lead beta resorcylate, 2.0 percent basic cupric salicylate, 0.5 percent 2-nitrodiphenylamine, and 0.02 percent carbon black.</description><language>eng</language><subject>CHEMISTRY ; EXPLOSIVES ; EXPLOSIVES OR THERMIC COMPOSITIONS ; MANUFACTURE THEREOF ; MATCHES ; METALLURGY ; USE OF SINGLE SUBSTANCES AS EXPLOSIVES</subject><creationdate>1975</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=19750415&DB=EPODOC&CC=US&NR=3878003A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19750415&DB=EPODOC&CC=US&NR=3878003A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LO PRESTI; ARTHUR</creatorcontrib><creatorcontrib>BAUMANN; ROBERT P</creatorcontrib><title>Composite double base propellant with HMX oxidizer</title><description>1. A solid propellant composition comprising, by weight, 50 percent cyclotetramethylene tetranitramine, 17.7 percent nitrocellulose, 22.1 percent nitroglycerin, 5.2 percent triacetin, 0.5 percent diethylphthalate, 2.0 percent basic lead beta resorcylate, 2.0 percent basic cupric salicylate, 0.5 percent 2-nitrodiphenylamine, and 0.02 percent carbon black.</description><subject>CHEMISTRY</subject><subject>EXPLOSIVES</subject><subject>EXPLOSIVES OR THERMIC COMPOSITIONS</subject><subject>MANUFACTURE THEREOF</subject><subject>MATCHES</subject><subject>METALLURGY</subject><subject>USE OF SINGLE SUBSTANCES AS EXPLOSIVES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1975</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDByzs8tyC_OLElVSMkvTcpJVUhKLE5VKCjKL0jNyUnMK1EozyzJUPDwjVDIr8hMyaxKLeJhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfGhwcYW5hYGBsaOxoRVAAAiRCte</recordid><startdate>19750415</startdate><enddate>19750415</enddate><creator>LO PRESTI; ARTHUR</creator><creator>BAUMANN; ROBERT P</creator><scope>EVB</scope></search><sort><creationdate>19750415</creationdate><title>Composite double base propellant with HMX oxidizer</title><author>LO PRESTI; ARTHUR ; BAUMANN; ROBERT P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US3878003A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1975</creationdate><topic>CHEMISTRY</topic><topic>EXPLOSIVES</topic><topic>EXPLOSIVES OR THERMIC COMPOSITIONS</topic><topic>MANUFACTURE THEREOF</topic><topic>MATCHES</topic><topic>METALLURGY</topic><topic>USE OF SINGLE SUBSTANCES AS EXPLOSIVES</topic><toplevel>online_resources</toplevel><creatorcontrib>LO PRESTI; ARTHUR</creatorcontrib><creatorcontrib>BAUMANN; ROBERT P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LO PRESTI; ARTHUR</au><au>BAUMANN; ROBERT P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Composite double base propellant with HMX oxidizer</title><date>1975-04-15</date><risdate>1975</risdate><abstract>1. A solid propellant composition comprising, by weight, 50 percent cyclotetramethylene tetranitramine, 17.7 percent nitrocellulose, 22.1 percent nitroglycerin, 5.2 percent triacetin, 0.5 percent diethylphthalate, 2.0 percent basic lead beta resorcylate, 2.0 percent basic cupric salicylate, 0.5 percent 2-nitrodiphenylamine, and 0.02 percent carbon black.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_US3878003A |
| source | esp@cenet |
| subjects | CHEMISTRY EXPLOSIVES EXPLOSIVES OR THERMIC COMPOSITIONS MANUFACTURE THEREOF MATCHES METALLURGY USE OF SINGLE SUBSTANCES AS EXPLOSIVES |
| title | Composite double base propellant with HMX oxidizer |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T12%3A23%3A23IST&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=LO%20PRESTI;%20ARTHUR&rft.date=1975-04-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS3878003A%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 |