GUIDED MISSILE (MODIFICATIONS)
FIELD: armament. ^ SUBSTANCE: the guided missile, having a canard aerodynamic configuration, has a cylindrical body, stabilizer and aerodynamic control surfaces. A circular pylon made of a ring plate coupled to the body by plane-surface plates in installed on the body nose before the control surface...
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creator | SHIPUNOV ARKADIJ GEORGIEVICH GOLOMIDOV BORIS ALEKSANDROVICH STEPANICHEV IGOR' VENIAMINOVICH MOROZOV VLADIMIR IVANOVICH GUSAROV NIKOLAJ IVANOVICH |
description | FIELD: armament. ^ SUBSTANCE: the guided missile, having a canard aerodynamic configuration, has a cylindrical body, stabilizer and aerodynamic control surfaces. A circular pylon made of a ring plate coupled to the body by plane-surface plates in installed on the body nose before the control surface. According to the other modification, a plane-surface pylon made of plates cantilever fastened an the body at an angle of 45 deg. relative to the plane of the control surface cantilevers is installed on the guided missile nose behind the control surface. ^ EFFECT: enhanced efficiency of the guided missile. ^ 2 cl, 8 dwg |
format | Patent |
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A circular pylon made of a ring plate coupled to the body by plane-surface plates in installed on the body nose before the control surface. According to the other modification, a plane-surface pylon made of plates cantilever fastened an the body at an angle of 45 deg. relative to the plane of the control surface cantilevers is installed on the guided missile nose behind the control surface. ^ EFFECT: enhanced efficiency of the guided missile. ^ 2 cl, 8 dwg</description><language>eng ; rus</language><subject>AMMUNITION ; BLASTING ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2007</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=20070110&DB=EPODOC&CC=RU&NR=2291381C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20070110&DB=EPODOC&CC=RU&NR=2291381C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SHIPUNOV ARKADIJ GEORGIEVICH</creatorcontrib><creatorcontrib>GOLOMIDOV BORIS ALEKSANDROVICH</creatorcontrib><creatorcontrib>STEPANICHEV IGOR' VENIAMINOVICH</creatorcontrib><creatorcontrib>MOROZOV VLADIMIR IVANOVICH</creatorcontrib><creatorcontrib>GUSAROV NIKOLAJ IVANOVICH</creatorcontrib><title>GUIDED MISSILE (MODIFICATIONS)</title><description>FIELD: armament. ^ SUBSTANCE: the guided missile, having a canard aerodynamic configuration, has a cylindrical body, stabilizer and aerodynamic control surfaces. A circular pylon made of a ring plate coupled to the body by plane-surface plates in installed on the body nose before the control surface. According to the other modification, a plane-surface pylon made of plates cantilever fastened an the body at an angle of 45 deg. relative to the plane of the control surface cantilevers is installed on the guided missile nose behind the control surface. ^ EFFECT: enhanced efficiency of the guided missile. ^ 2 cl, 8 dwg</description><subject>AMMUNITION</subject><subject>BLASTING</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2007</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBzD_V0cXVR8PUMDvb0cVXQ8PV38XTzdHYM8fT3C9bkYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxQaFGRpaGxhaGzobGRCgBAGWkIOs</recordid><startdate>20070110</startdate><enddate>20070110</enddate><creator>SHIPUNOV ARKADIJ GEORGIEVICH</creator><creator>GOLOMIDOV BORIS ALEKSANDROVICH</creator><creator>STEPANICHEV IGOR' VENIAMINOVICH</creator><creator>MOROZOV VLADIMIR IVANOVICH</creator><creator>GUSAROV NIKOLAJ IVANOVICH</creator><scope>EVB</scope></search><sort><creationdate>20070110</creationdate><title>GUIDED MISSILE (MODIFICATIONS)</title><author>SHIPUNOV ARKADIJ GEORGIEVICH ; GOLOMIDOV BORIS ALEKSANDROVICH ; STEPANICHEV IGOR' VENIAMINOVICH ; MOROZOV VLADIMIR IVANOVICH ; GUSAROV NIKOLAJ IVANOVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2291381C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2007</creationdate><topic>AMMUNITION</topic><topic>BLASTING</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>SHIPUNOV ARKADIJ GEORGIEVICH</creatorcontrib><creatorcontrib>GOLOMIDOV BORIS ALEKSANDROVICH</creatorcontrib><creatorcontrib>STEPANICHEV IGOR' VENIAMINOVICH</creatorcontrib><creatorcontrib>MOROZOV VLADIMIR IVANOVICH</creatorcontrib><creatorcontrib>GUSAROV NIKOLAJ IVANOVICH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SHIPUNOV ARKADIJ GEORGIEVICH</au><au>GOLOMIDOV BORIS ALEKSANDROVICH</au><au>STEPANICHEV IGOR' VENIAMINOVICH</au><au>MOROZOV VLADIMIR IVANOVICH</au><au>GUSAROV NIKOLAJ IVANOVICH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GUIDED MISSILE (MODIFICATIONS)</title><date>2007-01-10</date><risdate>2007</risdate><abstract>FIELD: armament. ^ SUBSTANCE: the guided missile, having a canard aerodynamic configuration, has a cylindrical body, stabilizer and aerodynamic control surfaces. A circular pylon made of a ring plate coupled to the body by plane-surface plates in installed on the body nose before the control surface. According to the other modification, a plane-surface pylon made of plates cantilever fastened an the body at an angle of 45 deg. relative to the plane of the control surface cantilevers is installed on the guided missile nose behind the control surface. ^ EFFECT: enhanced efficiency of the guided missile. ^ 2 cl, 8 dwg</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; rus |
recordid | cdi_epo_espacenet_RU2291381C1 |
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subjects | AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | GUIDED MISSILE (MODIFICATIONS) |
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