GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR Russian patent published in 1997 - IPC

Abstract RU 2074382 C1

FIELD: armament, in particular, rocket engineering. SUBSTANCE: the distribution device in guided missile aerodynamic control actuator has base 9 with nozzle part 10. Control electromagnet 4 is installed in the central part of base 9. Gap 18 is provided between the internal wall of the nozzle part and casing of control electromagnet 4. Armature-shutter 14 is made in the form of a disk with a central hole and ducts 19. EFFECT: improved design. 3 dwg

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RU 2 074 382 C1

Authors

Shipunov A.G.

Zybin I.M.

Shornikov E.E.

Fimushkin V.S.

Dates

1997-02-27—Published

1994-06-07—Filed