发明名称 METHOD FOR SEPARATION OF BALLISTIC CAP OF GUIDED MISSILE AND BALLISTIC CAP FOR ITS REALIZATION
摘要 FIELD: armament, in particular, guided missiles and rockets. ^ SUBSTANCE: the guided missile ballistic cap has a body, separation device with a separation chamber, powder charge placed in a high-pressure chamber communicating with the separation chamber through an opening. Installed in the separation chamber is a partition with exhaust-gas ducts separating the separation chamber into two cavities, with an additional charge of fine-grained powder, mainly pyroxylin one, located in one of them communicating with the high-pressure chamber through an opening. A metal screen is installed between the additional charge and the partition, whose cell dimension is less than the linear dimension of the powder grain of the additional charge. The additional charge of fine-grained powder is installed separately from the powder charge limiting its displacement in the direction of motion of the ballistic cap. ^ EFFECT: enhanced reliability of separation of the guided missile ballistic cap within a wide temperature range of operation at guided missile flight speeds exceeding 2-3M. ^ 2 cl, 1 dwg
申请公布号 RU2246690(C1) 申请公布日期 2005.02.20
申请号 RU20040101455 申请日期 2004.01.19
申请人 发明人 KAPUSTIN A.S.;KOLIKOV V.A.;KOLONITSKIJ E.K.;KOSJAKIN V.M.;KUZNETSOV V.M.;PAVLOV A.M.;SHVYKIN JU.S.;JUDINA JU.V.
分类号 F42B15/00 主分类号 F42B15/00
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