Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1987-02-27
1988-10-11
Barefoot, Galen L.
Aeronautics and astronautics
Spacecraft
Attitude control
74572, 244164, B64G 128
Patent
active
047765410
ABSTRACT:
Large angular control moments and torques are developed by controllably circulating a relatively small mass of liquid (22) through small diameter pipes (20) describing a large diameter loop (15f,a,b). The loop (15), by thus generating and storing angular momentum, can thereby provide efficient cancellation of periodic, non-accumulating, externally induced rotational disturbances. The loop (15) is preferably located on or near the periphery of a structure (10) which is to be thus stabilized.
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patent: 4212443 (1980-07-01), Duncan et al.
patent: 4230294 (1980-10-01), Pistiner
patent: 4288051 (1981-09-01), Goschell
patent: 4504033 (1985-03-01), Engelking
patent: 4579302 (1986-04-01), Schneider et al.
Barefoot Galen L.
Fein Edward K.
Manning John R.
Schlorff Russell E.
The United States of America as represented by the Administrator
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