Descripción
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Among the many advantages of the recently proposed ion beam shepherd (IBS) debris removal technique is the capability to deal with multiple targets in a single mission. A preliminary analysis is here conducted in order to estimate the cost in terms of spacecraft mass and total mission time to remove multiple large-size upper stages of the Zenit family. Zenit-2 upper stages are clustered at 71 degrees inclination around 850 km altitude in low Earth orbit. It is found that a removal of two targets per year is feasible with a modest size spacecraft. The most favorable combinations of targets are outlined. | |
Internacional
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Si |
Nombre congreso
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6th European Conference on Space Debris |
Tipo de participación
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960 |
Lugar del congreso
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European Space Operations Centre, Darmstadt, Germany |
Revisores
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Si |
ISBN o ISSN
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1609042X |
DOI
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Fecha inicio congreso
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22/04/2013 |
Fecha fin congreso
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25/04/2013 |
Desde la página
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1 |
Hasta la página
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5 |
Título de las actas
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Proceedings of the 6th European Conference on Space Debris |