GUIDED MISSILE WARHEAD Russian patent published in 1997 - IPC

Abstract RU 2072504 C1

FIELD: rocket engineering. SUBSTANCE: leading shaped charge 1 is installed in fairing 3 on base 5. Internal contact 4 in front part 6 is cone-shaped or ogival, rear part 7 is cylindrical. The ratio of parts 6 and 7 is 1:(1.5 to 2.5). Reinforced plastic flange 8 is formed on the end of internal contact 4. Internal contact 4 is attached to base 5 by screws 9. EFFECT: improved design. 1 dwg

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RU 2 072 504 C1

Authors

Shipunov A.G.

Zakharov L.G.

Zybin I.M.

Dates

1997-01-27—Published

1994-05-31—Filed