Dual spin zero momentum satellite system

Details Dual spin zero momentum satellite system Dual spin zero momentum satellite system

1999-04-07

2000-11-28

Eldred, J. Woodrow

Aeronautics and astronautics

Spacecraft

Attitude control

244165, B64G 128

Patent

active

061524026

ABSTRACT:
An attitude control system for a spacecraft which includes a bearing power and transfer assembly. The bearing power and transfer assembly is disposed between a first body and a second body. The first body and the second body are counter-rotated with respect to each other by the bearing and power transfer assembly such that the overall spacecraft momentum about the spin axis of the bearing and power transfer assembly is nominally zero.

REFERENCES:
patent: 3877662 (1975-04-01), Reiter et al.
patent: 4723735 (1988-02-01), Eisenhaure et al.
patent: 4735382 (1988-04-01), Pinson
patent: 5014936 (1991-05-01), Nauck
patent: 5067673 (1991-11-01), Fong
patent: 5441222 (1995-08-01), Rosen
patent: 5611505 (1997-03-01), Smay

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