GUIDED SHELL LAUNCH METHOD AND THE GUIDED SHELL Russian patent published in 2008 - IPC F42B10/20 F42B15/01 

Abstract RU 2324142 C2

FIELD: weapons and ammunition; rocketry.

SUBSTANCE: shell contains leading cumulative charge, main payload, steering drive unit, placed between them, steer opening mechanism with electroignitor, stabiliser blades. Steer opening mechanism and electroignitor are located in the steering drive unit base, at that, electroignitor is done with powder hinge, which provides steer opening delay after stabiliser blades are opened, equal to 0.25-0.35 sec.

EFFECT: firing efficiency increase.

2 cl, 4 dwg

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RU 2 324 142 C2

Authors

Shipunov Arkadij Georgievich

Zakharov Lev Grigor'Evich

Zybin Igor' Mikhajlovich

Tjurin Vladimir Fedorovich

Fimushkin Valerij Sergeevich

Dates

2008-05-10Published

2006-04-26Filed