Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Reexamination Certificate
2006-08-10
2008-10-07
Gregory, Bernarr E (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
C244S003100, C102S473000, C102S501000, C102S200000, C102S206000, C102S207000
Reexamination Certificate
active
07431237
ABSTRACT:
A projectile has the ability to generate and provide power to components located in two sections of the projectile which have relative rotation to each other. The projectile has a pair of generators allowing the powering of components in two sections. The projectile has a force-producing device for altering the direction of the projectile as the projectile moves along the longitudinal axis of the projectile and the relative rotational position of the force-producing device on the projectile is controlled by a generator.
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Marshall John Adams
Mock M. Robert
Sweer Grant Allen
BainwoodHuang
Gregory Bernarr E
HR Textron Inc.
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