Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Reexamination Certificate
2008-12-17
2011-11-01
Gregory, Bernarr (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
C244S003100, C244S003150, C244S003210, C244S003240, C244S003270, C244S003280
Reexamination Certificate
active
08049149
ABSTRACT:
Methods and apparatus for an air brake system for a projectile according to various aspects of the present invention comprises a pivot and a protrusion mounted on the pivot. The protrusion is adapted to selectively translate outward from the projectile around a translation axis that is parallel to the longitudinal axis of the projectile. The methods and apparatus may further operate in conjunction with an actuation system engaging the protrusion, wherein the actuation system is configured to selectively facilitate the translation of the protrusion.
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European Patent Office, International Searching Authority, “International Search Report,” mailed Sep. 10, 2009; International Application No. PCT/US2009/043826, international filing date May 13, 2009.
Eisenbacher Matthew O.
Fink Jason J.
Geswender Chris E.
Streeter James D.
Zamora Matthew A.
Gregory Bernarr
Ingrassia Fisher & Lorenz P.C.
Raytheon Company
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