System and method for deployment and actuation

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Reexamination Certificate

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Details

C244S003100, C244S003270, C244S003280, C244S075100, C244S099200, C244S099300

Reexamination Certificate

active

07906749

ABSTRACT:
A mechanical deployment and actuation system may comprise a rotation module, a pinion module, a rack module, and a bevel module. The rotation module may be configured to couple to a housing and rotate about the principal axis of the rotation module relative to the housing. The pinion module may be configured to couple to the rotation module and selectively rotate about the principal axis of the pinion module relative to the rotation module. The rack module may be configured to dynamically couple to the pinion module and translate along the principal axis of the rack module in response to rotation of the pinion module. The bevel module may be configured to couple to the rotation module and selectively rotate the rotation module, wherein rotation of the rotation module rotates about the principal axis of the rotation module, the rack module, and the pinion module.

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patent: 4336914 (1982-06-01), Thomson
patent: 6347782 (2002-02-01), Gill
patent: 6726147 (2004-04-01), Perini et al.
patent: 7185847 (2007-03-01), Bouchard et al.

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