NASA NTRS ยท 19780007549
Magnetic bearings for instruments in the space environment
Abstract
A magnetic bearing development is documented, which has been successfully applied to support a 0.9 kg - 19 cm diameter rotor in 5 degrees of freedom, with fully controlled drive capability to plus or minus 200 rad/s in the other axis. The construction details are described and illustrated. Performance data on five design variations are presented which extend the load capacity to 8 kilograms at which point the bearing element on the rotor is less than one-half of 1 percent of the total load capacity.
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Studer, P. A.. 1978-01-01. Magnetic bearings for instruments in the space environment. https://ntrs.nasa.gov/citations/19780007549
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