An universal system to de-orbit satellites at end of life
Data(s) |
2012
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Resumo |
A 3-year Project financed by the European Commission is aimed at developing a universal system to de-orbit satellites at their end of life, as a fundamental contribution to limit the increase of debris in the Space environment. The operational system involves a conductive tapetether left bare to establish anodic contact with the ambient plasma as a giant Langmuir probe. The Project will size the three disparate dimensions of a tape for a selected de-orbit mission and determine scaling laws to allow system design for a general mission. Starting at the second year, mission selection is carried out while developing numerical codes to implement control laws on tether dynamics in/off the orbital plane; performing numerical simulations and plasma chamber measurements on tether-plasma interaction; and completing design of subsystems: electronejecting plasma contactor, power module, interface elements, deployment mechanism, and tether-tape/end-mass. This will be followed by subsystems manufacturing and by currentcollection, free-fall, and hypervelocity impact tests. |
Formato |
application/pdf |
Identificador | |
Idioma(s) |
eng |
Publicador |
E.T.S.I. Aeronáuticos (UPM) |
Relação |
http://oa.upm.es/30313/1/JSTS2012.pdf https://www.jstage.jst.go.jp/article/jsts/26/1/26_1_21/_article info:eu-repo/semantics/altIdentifier/doi/10.11230/jsts.26.1_21 |
Direitos |
http://creativecommons.org/licenses/by-nc-nd/3.0/es/ info:eu-repo/semantics/openAccess |
Fonte |
The Journal of Space Technology and Science, ISSN 0911-551X, 2012, Vol. 26, No. 1 |
Palavras-Chave | #Aeronáutica #Física |
Tipo |
info:eu-repo/semantics/article Artículo NonPeerReviewed |