An integrated micro HTS system for energy storage and attitude control for three-axis stabilized nanosatellites
This paper presents the development of an integrated micro high-temperature superconductor system for energy storage and attitude control of three-axis stabilized nano satellites. The micro HTS system consists of a flywheel/rotor, motor/generator, motor electronics, and a cooling system. The flywhee...
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Veröffentlicht in: | IEEE transactions on applied superconductivity 2005-06, Vol.15 (2), p.2324-2327 |
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Sprache: | eng |
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