Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Reexamination Certificate
2006-02-28
2006-02-28
Barefoot, Galen (Department: 3644)
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
C244S049000
Reexamination Certificate
active
07004425
ABSTRACT:
A missile to be fired from a barrel contains a tail, a tail sleeve attached to the tail, a stop element fixed to the tail sleeve, and a movable structural part disposed at the tail. Fin assembly wings are provided and are to be released from a subcaliber launch position to an overcaliber functional position by the movable structural part moving toward the stop element through a given distance. A pressure area is disposed between the tail end surface and the movable structural part. A propellant gas enters the pressure area during the firing of the missile, for moving the movable structural part away from the tail end surface against the stop element after firing. Bearing shafts are supported by the tail sleeve, the fin assembly wings are configured as a wrap around tail fin assembly held about the bearing shafts.
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Mochizuki Makoto
Okada Shin-ichi
Okawa Sadao
Shinomiya Masato
Barefoot Galen
Diehl Munitionssysteme GmbH & Co. KG
Greenberg Laurence A.
Locher Ralph E.
Stemer Werner H.
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