Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Reexamination Certificate
2008-07-29
2010-06-01
Collins, Timothy D (Department: 3643)
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
C244S099800
Reexamination Certificate
active
07728267
ABSTRACT:
Methods and apparatus for systems having deployable elements according to various aspects of the present invention comprise a system including a deployable surface and an adaptive actuator including a polymer foam. In one embodiment, the system comprises a vehicle including a deployable wing comprising an exterior surface. The exterior surface may be adjusted by adjusting the shape, size, position, and/or orientation of the adaptive actuator.
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Clark Jamie W.
Sanderson Terry M.
Collins Timothy D
Raytheon Company
Renner , Otto, Boisselle & Sklar, LLP
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