GUIDED MISSILE NOSE CONE Russian patent published in 1997 - IPC

Abstract RU 2089834 C1

FIELD: rocketry. SUBSTANCE: guided missile nose cone contains leading shaped charge 1, control actuator unit 2, fairing shaped charge 1, control actuator unit 2, fairing 3 with air-intake opening 5, contact 4 with the air-intake opening 9. Filter screen 6 is secured in contact 4. Partition 10 of insulating material is positioned in the middle part between the outer surface of contact 4 and inner surface of fairing 3. EFFECT: improved design. 1 dwg

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RU 2 089 834 C1

Authors

Zybin I.M.

Fimushkin V.S.

Dates

1997-09-10—Published

1995-06-28—Filed