Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1995-06-23
1997-04-22
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
102385, 102517, 102521, 244 31, F42B 1006
Patent
active
056223358
ABSTRACT:
A tail piece for a projectile includes at least three fins connected to either the projectile itself or a bracket connected to the projectile. Each fin is linked to the projectile/bracket by at least one fastening foot that cooperates with at least one recess of the projectile/bracket.
REFERENCES:
patent: 3392934 (1968-07-01), Daniels
patent: 4004514 (1977-01-01), Daniels
Abstract of EP 0 300 373, Jan. 1989.
Beauvais Fran.cedilla.ois
Millet Yves
Trouillot Christian
Giat Industries
Tudor Harold J.
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