GUIDED MISSILE CONTROL ACTUATOR Russian patent published in 1995 - IPC

Abstract RU 2046060 C1

FIELD: control system of flying vehicles. SUBSTANCE: guided missile control actuator has torus servo unit connected with control surfaces; provided in housing in plane perpendicular to axis of rotation of control surfaces are two torus chambers where piston is arranged in spaced relation. Piston is made in form of two disks connected with rod and provided with central hole for receiving the axle of control surfaces. EFFECT: enhanced reliability. 2 dwg

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RU 2 046 060 C1

Authors

Zybin I.M.

Dates

1995-10-20—Published

1992-12-07—Filed