Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1980-12-22
1983-05-24
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
F42B 1332
Patent
active
043846912
ABSTRACT:
A missile disposed for launching from a telescoping launcher having inner d outer sections. The missile is provided with fins folded along the body. A resilient spring clip member is carried on each said fin and engages the inner surfaces of the launcher sections as the missile traverses the launcher to retain the fins in folded position in the launcher.
REFERENCES:
patent: 3690595 (1972-09-01), Rusbach
patent: 3754726 (1973-08-01), Rusbach
patent: 3819132 (1974-06-01), Rusbach
patent: 3918664 (1975-11-01), Grosswendt
Edelberg Nathan
Gibson Robert P.
Hilton Harold W.
The United States of America as represented by the Secretary of
Tudor Harold J.
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