Micro Satellite Orbital Boost by Electrodynamic Tethers
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DOI: 10.3390/mi12080916
Abstract: In this manuscript, a method for maneuvering a spacecraft using electrically charged tethers is explored. The spacecraft’s velocity vector can be modified by interacting with Earth’s magnetic field. Through this method, a spacecraft can maintain… read more here.
Keywords: orbital boost; spacecraft; satellite orbital; boost electrodynamic ... See more keywords