Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1977-11-29
1979-06-19
Pendegrass, Verlin R.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
244 329, F42B 1322
Patent
active
041584473
ABSTRACT:
A device for providing fold out fins for stabilizing projectiles or missi which may be tube-launched. The missile is provided with a tubular element or cup which has a plurality of slots defining fin-like stabilizing flaps. The slots extend circumferentially around two sides of the flaps; a third slot interconnects the circumferential slots, while a fourth side is unslotted. Since the tubular element is in fluid communication with the pressure within the launcher, the stabilizing flaps or fins expand outwardly into position about the fourth unslotted side as the missile or the projectile leaves the launcher.
REFERENCES:
patent: 3031967 (1962-05-01), Jasse
patent: 3072055 (1963-01-01), Ross
patent: 3165281 (1965-01-01), Gohlke
patent: 3580529 (1971-05-01), Suter
patent: 3589645 (1971-06-01), Haglund
Humphries Waymon
Nahas Joseph A.
Beers R. F.
Pendegrass Verlin R.
Sciascia R. S.
Sheinbein Sol
The United States of America as represented by the Secretary of
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