Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1980-02-25
1982-09-28
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
102385, 244 321, F42B 1516
Patent
active
043515037
ABSTRACT:
Stabilized ballistic projectiles of the explosive type (e.g. artillery and mortar shells, bombs) are described including a plurality of stabilizing fins symmetrically arranged around the nose of the projectile well forward of its center of mass and pivotable on axes at right angles to the projectile axis, the leading edge of each fin, and the pivot axis of each fin, being located with respect to the foremost point of the projectile, inclusive of its stabilizing fins, a distance which is substantially less than the length of the fin.
REFERENCES:
patent: 1316296 (1919-09-01), Gathmann
patent: 2380278 (1945-07-01), Weissman
patent: 2433234 (1947-12-01), McHugh
patent: 2494026 (1950-01-01), Anderson
patent: 2752850 (1956-07-01), Warner et al.
patent: 3195462 (1965-07-01), Petre
patent: 3196794 (1965-07-01), Meade
patent: 3658004 (1972-04-01), Blair
Barish Benjamin J.
Tudor Harold J.
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