发明名称 SHELL WITH VOLUME-DETONATING MIXTURE
摘要 FIELD: weapons and ammunition. ^ SUBSTANCE: rocket shell includes head part, military part, cruise engine, axial channel, translating charge, bottom detonator, dispersing charge and retarder of initiating charge. Military part includes two dispersing charges, bottom and head ones, which are located coaxially in the form of piston group. Dispersing charges provide optimum exit of fuel-air mixture to atmosphere at simultaneous actuation. ^ EFFECT: maximum killing effectiveness of area targets with shell. ^ 1 dwg
申请公布号 RU2426064(C1) 申请公布日期 2011.08.10
申请号 RU20090141767 申请日期 2009.11.11
申请人 FEDERAL'NOE GOSUDARSTVENNOE UCHREZHDENIE "33 TSENTRAL'NYJ NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT" MINISTERSTVA OBORONY ROSSIJSKOJ FEDERATSII 发明人 BATRAKOV ANATOLIJ MIKHAJLOVICH;GRININA VERA ALEKSEEVNA;EGOROV EVGENIJ VIKTOROVICH;EGOROV KONSTANTIN VIKTOROVICH;URJADOV DMITRIJ BORISOVICH;KHARITONOV MAKSIM ALEKSANDROVICH;KHOMENKO MAKSIM ALEKSANDROVICH
分类号 F42B12/52 主分类号 F42B12/52
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