Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Reexamination Certificate
2007-06-05
2007-06-05
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
C244S003290, C102S473000
Reexamination Certificate
active
10907301
ABSTRACT:
This disclosure relates to a method and an arrangement for low or non-rotating artillery shells fired from launch weaponry, and which introduces a portion of the barrel pressure built up in the barrel during the launch phase into a chamber arranged in the low or non-rotating artillery shell which is delimited in at least one direction by an element which is movable relative to the rest of the shell when a differential pressure between the chamber and the external environment of the shell is sufficient to move the element. The moveable element may be a protective casing covering fins of the artillery shell.
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Hellman Ulf
Holmqvist Ulf
Johnsson Stig
BAE Systems Bofors AB
Connolly Bove & Lodge & Hutz LLP
Dinh Tien
Hume Larry J.
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