Low cost deployment system and method for airborne object

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

Reexamination Certificate

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C244S003270

Reexamination Certificate

active

08058597

ABSTRACT:
A deployment system is provided for utilization onboard an airborne object including a deployable element. In one embodiment, the deployment system includes a circumferential restraint and a release mechanism mounted to the airborne object. The circumferential restraint is disposed at least partially around the airborne object in a constraining position wherein the circumferential restraint prevents deployment of the deployable element. The release mechanism normally resides in a first position in which the release mechanism maintains the circumferential restraint in the constraining position. The release mechanism is movable to a second position to release the circumferential restraint from the constraining position and permit deployment of the deployable element.

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International Searching Authority, European Patent Office, “International search Report,” mailed Jul. 21, 2010; International Application No. PCT/US2010/032594, filed Apr. 27, 2010.
USPTO “Non-Final Office Action” mailed Jun. 9, 2011; U.S. Appl. No. 11/457,993, filed Jul. 17, 2006.

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