Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2005-11-01
2005-11-01
Gregory, Bernarr E. (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
C244S003100, C244S003150, C244S003240, C244S003270, C102S305000, C102S306000, C102S308000, C102S501000
Reexamination Certificate
active
06959893
ABSTRACT:
A projectile comprises an imaging seeker at a front of the projectile; a front warhead behind the imaging seeker; a power supply; an electronics unit connected to the power supply and comprising a microprocessor circuit board, a voltage regulator circuit board, an inertial measurement circuit board and a fuze and safe and arm circuit board, all electrically connected to each other, the microprocessor circuit board also being connected to the imaging seeker; a rear warhead, the front and rear warheads being electrically connected to the safe and arm circuit board; a rocket motor electrically connected to the electronics unit; foldable fins mounted at the rear of the projectile; a shell that encases the front warhead, the power supply, the electronics unit, the rear warhead and the rocket motor; and a maneuver mechanism disposed in the shell and electrically connected to the microprocessor circuit board.
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“Bill 2 Anti-Tank Guided weapon”; no author given; no date given; posted on the Internet at army-technology.com.
Chung Sung K.
Cincotta Tomas
Sadowski Lucian M.
Whiteside John H.
Gregory Bernarr E.
Moran John F.
Sachs Michael C.
The United States of America as represented by the Secretary of
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