GUIDED MISSILE Russian patent published in 2003 - IPC

Abstract RU 2199715 C2

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

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RU 2 199 715 C2

Authors

Zakharov L.G.

Zemlevskij O.V.

Kopylov Ju.D.

Kuznetsov Ju.M.

Parfenov P.P.

Dates

2003-02-27Published

2001-05-21Filed