Passive damper for spin stabilized projectiles

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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Details

244165, 244170, B64G 138

Patent

active

051392178

ABSTRACT:
A stabilizer comprised of a pair of toroidal fluid passages filled with a viscous fluid orthogonally mounted with respect to one another on a spin stabilized projectile. One torus is rigidly attached to the projectile and aligned with the x axis of the projectile and the other torus is similarly attached and aligned along the y axis.

REFERENCES:
patent: 2856142 (1958-10-01), Haviland
patent: 3034745 (1962-05-01), Stewart
patent: 3048350 (1962-08-01), Cutler
patent: 3433534 (1969-03-01), Mercer
patent: 3716206 (1973-02-01), Lynch et al.
patent: 3733923 (1973-05-01), Goodrich et al.
patent: 3758051 (1973-09-01), Williams

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