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Micro Satellite Orbital Boost by Electrodynamic Tethers

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 an orbit indefinitely by reboosting without the constr...

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Detalles Bibliográficos
Autores principales: Yao, Peter, Sands, Timothy
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8400572/
https://www.ncbi.nlm.nih.gov/pubmed/34442538
http://dx.doi.org/10.3390/mi12080916

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