ROCKET ARMAMENT LAUNCHABLE FROM A TUBULAR LAUNCHER WITH AN OUTSIDE LAUNCHER NON-IGNITION SECURING AND MOTOR SEPARATION DURING FLIGHT
Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight and a method to prevent the ignition of the armaments rocket even in the event of actuation of the armaments pyrotechnic assembly, which normally serves to eject the a...
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| creator | Guller, Evgeny Ziv, Jakov Tal, Nadav Teper, Yossi |
| description | Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight and a method to prevent the ignition of the armaments rocket even in the event of actuation of the armaments pyrotechnic assembly, which normally serves to eject the armament from the launcher and to ignite its rocket motor, wherein the armament comprises a gas dispersion assembly, which when the armament is not encased in the tubular launcher, prevents the ignition of the rocket motor even if the armaments pyrotechnic assembly is actuated; and a cutting and separation assembly that is actuated by the pressure of the rocket motor gases for mechanically cutting a structural connection between the rocket motor and the armaments effective payload and separate them during their flight. |
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and a cutting and separation assembly that is actuated by the pressure of the rocket motor gases for mechanically cutting a structural connection between the rocket motor and the armaments effective payload and separate them during their flight.</description><language>eng</language><subject>AMMUNITION ; AMMUNITION FUZES ; APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; ARMING OR SAFETY MEANS THEREFOR ; BLASTING ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; HARPOON GUNS ; HEATING ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2021</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=20210826&DB=EPODOC&CC=US&NR=2021262756A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210826&DB=EPODOC&CC=US&NR=2021262756A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Guller, Evgeny</creatorcontrib><creatorcontrib>Ziv, Jakov</creatorcontrib><creatorcontrib>Tal, Nadav</creatorcontrib><creatorcontrib>Teper, Yossi</creatorcontrib><title>ROCKET ARMAMENT LAUNCHABLE FROM A TUBULAR LAUNCHER WITH AN OUTSIDE LAUNCHER NON-IGNITION SECURING AND MOTOR SEPARATION DURING FLIGHT</title><description>Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight and a method to prevent the ignition of the armaments rocket even in the event of actuation of the armaments pyrotechnic assembly, which normally serves to eject the armament from the launcher and to ignite its rocket motor, wherein the armament comprises a gas dispersion assembly, which when the armament is not encased in the tubular launcher, prevents the ignition of the rocket motor even if the armaments pyrotechnic assembly is actuated; and a cutting and separation assembly that is actuated by the pressure of the rocket motor gases for mechanically cutting a structural connection between the rocket motor and the armaments effective payload and separate them during their flight.</description><subject>AMMUNITION</subject><subject>AMMUNITION FUZES</subject><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>ARMING OR SAFETY MEANS THEREFOR</subject><subject>BLASTING</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyrEKwjAUheEuDqK-wwXngo2o822aNsEmkdsbHEuROIkW6iP44BYtuDodON8_T17k5VExIFm0yjHUGJzUmNcKSvIWEDjkoUaaRBGcDWtABz5wYwr1A-ddaipn2HgHjZKBjKvGsgDr2dN4nZDwo8XXytpUmpfJ7NrdhriadpGsS8VSp7F_tHHou0u8x2cbGrERmdiLw26P2fa_6g1V5j5H</recordid><startdate>20210826</startdate><enddate>20210826</enddate><creator>Guller, Evgeny</creator><creator>Ziv, Jakov</creator><creator>Tal, Nadav</creator><creator>Teper, Yossi</creator><scope>EVB</scope></search><sort><creationdate>20210826</creationdate><title>ROCKET ARMAMENT LAUNCHABLE FROM A TUBULAR LAUNCHER WITH AN OUTSIDE LAUNCHER NON-IGNITION SECURING AND MOTOR SEPARATION DURING FLIGHT</title><author>Guller, Evgeny ; Ziv, Jakov ; Tal, Nadav ; Teper, Yossi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2021262756A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2021</creationdate><topic>AMMUNITION</topic><topic>AMMUNITION FUZES</topic><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>ARMING OR SAFETY MEANS THEREFOR</topic><topic>BLASTING</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Guller, Evgeny</creatorcontrib><creatorcontrib>Ziv, Jakov</creatorcontrib><creatorcontrib>Tal, Nadav</creatorcontrib><creatorcontrib>Teper, Yossi</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Guller, Evgeny</au><au>Ziv, Jakov</au><au>Tal, Nadav</au><au>Teper, Yossi</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ROCKET ARMAMENT LAUNCHABLE FROM A TUBULAR LAUNCHER WITH AN OUTSIDE LAUNCHER NON-IGNITION SECURING AND MOTOR SEPARATION DURING FLIGHT</title><date>2021-08-26</date><risdate>2021</risdate><abstract>Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight and a method to prevent the ignition of the armaments rocket even in the event of actuation of the armaments pyrotechnic assembly, which normally serves to eject the armament from the launcher and to ignite its rocket motor, wherein the armament comprises a gas dispersion assembly, which when the armament is not encased in the tubular launcher, prevents the ignition of the rocket motor even if the armaments pyrotechnic assembly is actuated; and a cutting and separation assembly that is actuated by the pressure of the rocket motor gases for mechanically cutting a structural connection between the rocket motor and the armaments effective payload and separate them during their flight.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_epo_espacenet_US2021262756A1 |
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| subjects | AMMUNITION AMMUNITION FUZES APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ARMING OR SAFETY MEANS THEREFOR BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | ROCKET ARMAMENT LAUNCHABLE FROM A TUBULAR LAUNCHER WITH AN OUTSIDE LAUNCHER NON-IGNITION SECURING AND MOTOR SEPARATION DURING FLIGHT |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T00%3A25%3A09IST&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=Guller,%20Evgeny&rft.date=2021-08-26&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2021262756A1%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 |