Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1993-01-11
1994-07-05
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
102388, 244 49, 244173, 343882, 343DIG2, F42B 1014
Patent
active
053260490
ABSTRACT:
A device, particularly a missile, includes a body having an appendage, e.g., a wing, normally folded in an inoperative position and to be unfolded to an operative position when the body is accelerated in the direction of the longitudinal axis of the body. The appendage is pivotally mounted about a first pivot axis extending perpendicularly to the longitudinal axis of the body, and also about a second pivot axis extending parallel to the longitudinal axis of the body. The center of gravity of the appendage is outwardly of the first pivot axis in the folded condition of the appendage such that the acceleration of the body produces a moment pivotting the appendage about the first pivot axis.
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Rom Hanan
Yehezkeli Oded
Friedman Mark M.
State of Israel - Ministry of Defense Rafael-Armament Developmen
Tudor Harold J.
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