发明名称 GUIDED MISSILE
摘要 FIELD: defense equipment, means for fighting with tanks and other small-sized targets, in particular, guided missiles spin-stabilized in the flight trajectory. SUBSTANCE: the described rolled missile has an actuating mechanism of the warhead destruction, airborne control equipment, gyro with a pulse rotary transducer, power source and a shift, register, whose sync input is connected to the output of the pulse rotary transducer. The guided missile uses a device for setting in the initial position, logic level source and a successively connected safety device and an electronic key, which would enhance the safety of the complex crew and efficiency of arming of the warhead with prevention of the influence of the guided missile flight speed on the range of removal of interlocking and enhance efficiency of warhead arming due to a high stability of arming for a near range of target destruction. EFFECT: enhanced efficiency of warhead arming at an enhanced safety of the crew. 1 dwg
申请公布号 RU2199715(C2) 申请公布日期 2003.02.27
申请号 RU20010113852 申请日期 2001.05.21
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTO;GUP KONSTRUKTO 发明人 ZAKHAROV L.G.;ZEMLEVSKIJ O.V.;KOPYLOV JU.D.;KUZNETSOV JU.M.;PARFENOV P.P.
分类号 F42B15/01;(IPC1-7):F42B15/01 主分类号 F42B15/01
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