发明名称 SAFETY-ACTUATING MECHANISM FOR WARHEADS OF ROCKET AMMUNITION
摘要 FIELD: technical devices for equipment of ammunition warheads with an on-board power source, mainly of guided rockets or missiles having of cruise engine. ^ SUBSTANCE: the safety-actuating mechanism is characterized by the fact that it has a double-acting electrical detonator for equipment of the main detonator of the ammunition warhead, firing arming system, standard fitting system, self-destruction system and a system of protection at non-standard situations. The self-destruction system has an inertia starting mechanism, electric igniter, pyrotechnical self-destruction track, primer cap and a burned-through gasket, and the system of protection at non-standard situations has a shutter, contact coupled to it, shunting double-acting electrical detonator and an inertia mechanism. ^ EFFECT: enhanced reliability and safety of operation of the ammunition in standard and non-standard conditions. ^ 3 cl, 5 dwg
申请公布号 RU2301960(C2) 申请公布日期 2007.06.27
申请号 RU20050121224 申请日期 2005.07.07
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "NAUCHNO-ISSLEDOVATEL'SKIJ TEKHNOLOGICHESKIJ INSTITUT IM.P.I.SNEGIREVA" 发明人 SHEVCHENKO ALEKSEJ MITROFANOVICH;SERDJUKOVA VALENTINA NIKOLAEVNA;SYZRANTSEV VJACHESLAV FEDOROVICH
分类号 F42C15/00 主分类号 F42C15/00
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