GUIDED MISSILE ACTUATOR ASSEMBLY Russian patent published in 1998 - IPC

Abstract RU 2101665 C1

FIELD: guided missiles. SUBSTANCE: guided missile actuator assembly has control actuators with a distribution device and an air intake installed on the base. A manifold serving at the same time as a receiver is installed on the base between the leading shaped charge and the fairing. The air intakes are made rotary for outlet behind the fairing contours through the grooves for control surfaces and communicate with the manifold inlets through flexible tubes. A filter is installed inside the manifold, and the manifold outlet communicates with the inlet of the distribution device of the control actuators. EFFECT: improved design. 2 cl, 3 dwg

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RU 2 101 665 C1

Authors

Zybin I.M.

Fimushkin V.S.

Golovanov N.S.

Dates

1998-01-10Published

1996-06-13Filed