发明名称 GUIDED MISSILE
摘要 FIELD: rocketry. SUBSTANCE: guided missile has the leading shaped charge and the main warhead with safety-and- actuating mechanisms, as well as the control actuator unit with coils of the polarized control electromagnet, and coil of two-wire communication line. The communication line coil is connected to the beginnings of the coils of the control electromagnet of the control actuator unit, and the ends of these coils are combined by a jumper and parallel- connected to the safety-and actuating mechanisms of the leasing shaped charge and the main warhead. EFFECT: enhanced reliability of the safety-and-actuating mechanisms and the missile on the whole. 2 dwg
申请公布号 RU2127417(C1) 申请公布日期 1999.03.10
申请号 RU19980104574 申请日期 1998.02.16
申请人 KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA 发明人 SHIPUNOV A.G.;TIKHONOV V.P.;ZAKHAROV L.G.;ZYBIN I.M.;BOEV I.V.
分类号 F42B15/00;(IPC1-7):F42B15/00 主分类号 F42B15/00
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