Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1984-09-24
1986-04-22
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
102388, 244 327, F42B 1332, F42B 15053, F42B 2520
Patent
active
045837031
ABSTRACT:
An orientation and stabilization device for a submunition is disclosed. A w profile cylindrical submunition body has a single fin attached thereto at an asymmetrically located position with respect to the central axis of the cylindrical body. The fin is tip weighted in such a way that, when the submunition falls through the air, a constant spin and vertical velocity is established, with the major axis of the cylindrical body disposed at an angle to the descent path.
REFERENCES:
patent: D137155 (1944-01-01), Lewis
patent: 2667352 (1954-01-01), Sepersky
patent: 2921404 (1960-01-01), Lescher
patent: 3273834 (1966-09-01), Bower
patent: 3353295 (1967-11-01), Downey
patent: 3604352 (1971-09-01), Bench
patent: 3691674 (1972-09-01), Thompson
patent: 4050381 (1977-09-01), Heinemann
patent: 4356770 (1982-11-01), Atanasoff et al.
Gibson Robert P.
Jordan Charles T.
Lane. Anthony T.
Sachs Michael C.
The United States of America as represented by the Secretary of
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