GUIDED MISSILE CONTROL ACTUATOR UNIT Russian patent published in 1999 - IPC

Abstract RU 2124697 C1

FIELD: missile weaponry. SUBSTANCE: control actuator unit has a casing, air intakes, filter, actuators. The filter is installed in a recess in the central part of the casing. The recess inlet communicates with air intakes through channels, and the outlet - with actuators. EFFECT: simplified design and enhanced reliability of control actuator unit. 1 dwg

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RU 2 124 697 C1

Authors

Babichev V.I.

Zybin I.M.

Fimushkin V.S.

Dates

1999-01-10—Published

1997-09-25—Filed