Numerical study of rocket upper stage deorbiting using passive electrodynamic tether drag
The purpose of this article is a numerical study of the possibility of deorbiting a rocket upper stage from low Earth orbit at EOM (end of mission) by means of passive electrodynamic tether drag. The article is structured as follows: the introduction presents the space debris problem in low Earth or...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2014-12-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/ionel_alexandru__vol_6_iss_4.pdf |