E-sail test payload of the ESTCube-1 nanosatellite

The scientific mission of ESTCube-1, launched in May 2013, is to measure the electric solar wind sail (E-sail) force in orbit. The experiment is planned to push forward the development of the E-sail, a propulsion method recently invented at the Finnish Meteorological Institute. The E-sail is based o...

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Veröffentlicht in:Proceedings of the Estonian Academy of Sciences 2014-01, Vol.63 (2S), p.210
Hauptverfasser: Envall, J, Janhunen, P, Toivanen, P, Pajusalu, M, Ilbis, E, Kalde, J, Averin, M, Kuuste, H, Laizans, K, Allik, V, Rauhala, T, Seppänen, H, Kiprich, S, Ukkonen, J, Haeggström, E, Kalvas, T, Tarvainen, O, Kauppinen, J, Nuottajärvi, A, Koivisto, H
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Sprache:eng
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Zusammenfassung:The scientific mission of ESTCube-1, launched in May 2013, is to measure the electric solar wind sail (E-sail) force in orbit. The experiment is planned to push forward the development of the E-sail, a propulsion method recently invented at the Finnish Meteorological Institute. The E-sail is based on extracting momentum from the solar wind plasma flow by using long thin electrically charged tethers. ESTCube-1 is equipped with one such tether, together with hardware capable of deploying and charging it. At the orbital altitude of ESTCube-1 there is no solar wind present. Instead, ESTCube-1 shall observe the interaction between the charged tether and the ionospheric plasma. The ESTCube-1 payload uses a 10-m, partly two-filament E-sail tether and a motorized reel on which it is stored. The tether shall be deployed from a spinning satellite with the help of centrifugal force.During the E-sail experiment the tether shall be charged to 500 V potential. Both positive and negative voltages shall be experimented with.
ISSN:1736-6046
1736-7530
DOI:10.3176/proc.2014.2S.02