Aeronautics and astronautics – Missile stabilization or trajectory control – Stabilized by rotation
Patent
1990-11-13
1991-07-02
Carone, Michael J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Stabilized by rotation
F42B 1008
Patent
active
H00009326
ABSTRACT:
The invention is a projectile stabilizing fin formed with a laterally exting flat, triangular shaped tab positioned so that one point of the triangle points in the direction of the intended projectile direction and tilted so that air flow will impinge on the tab surface and cause the projectile to spin. Such construction is particularly useful for projectiles launched from smooth bore guns at high Kinetic Energy.
Carone Michael J.
Costigan Edward F.
Goldberg Edward
Lane Anthony T.
The United States of America as represented by the Secretary of
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