2020
DOI: 10.15407/itm2020.01.056
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Features of the use of magnetic controls in a coarse stabilization of spacecraft with aeromagnetic deorbit systems

Abstract: The development of hybrid deorbit means for used spacecraft is a promising line in the elaboration of space debris mitigation technologies. The main objective of this line is a search for optimal solutions in the development of new means for spacecraft removal from near-Earth orbits with account for certain operating limitations on the use of existing deorbit systems. So the advantage of hybrid deorbit means lies in broadening the scope of application of modern deorbit systems by combining certain technical fe… Show more

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