GUIDED MISSILE Russian patent published in 1997 - IPC

Abstract RU 2092778 C1

FIELD: rocketry. SUBSTANCE: leading shaped charge 1 is installed on control actuator unit 2. Installed behind it are engine 4 with central passage 5 and main warhead 6. Installed in central passage 5 of engine 4 is a control electromagnet with distribution device 3 secured on the end of control actuator unit 2. EFFECT: improved design. 1 dwg

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RU 2 092 778 C1

Authors

Shipunov A.G.

Zakharov L.G.

Zybin I.M.

Fimushkin V.S.

Kopylov Ju.D.

Dates

1997-10-10—Published

1995-02-01—Filed