Feasibility analysis of LEO and GEO large space debris...

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Advances in Space Research 2020 / 9

Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout

Baranov, A.A., Grishko, D.A., Shcheglov, G.A., Sholmin, A.S., Stognii, M.V., Kamenev, N.D.
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Journal:
Advances in Space Research
DOI:
10.1016/j.asr.2020.09.005
Date:
September, 2020
File:
PDF, 1.76 MB
2020
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