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 |
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| creator | 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 |
| description | 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. |
| doi_str_mv | 10.3176/proc.2014.2S.02 |
| format | Article |
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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.</description><identifier>ISSN: 1736-6046</identifier><identifier>EISSN: 1736-7530</identifier><identifier>DOI: 10.3176/proc.2014.2S.02</identifier><language>eng</language><publisher>Tallinn: Teaduste Akadeemia Kirjastus (Estonian Academy Publishers)</publisher><ispartof>Proceedings of the Estonian Academy of Sciences, 2014-01, Vol.63 (2S), p.210</ispartof><rights>Copyright Teaduste Akadeemia Kirjastus (Estonian Academy Publishers) 2014</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a305t-6b89c78eaf4a64a45d8d2f825c20c0a444e87dde7812a49920b682e07fbb27183</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,860,27903,27904</link.rule.ids></links><search><creatorcontrib>Envall, J</creatorcontrib><creatorcontrib>Janhunen, P</creatorcontrib><creatorcontrib>Toivanen, P</creatorcontrib><creatorcontrib>Pajusalu, M</creatorcontrib><creatorcontrib>Ilbis, E</creatorcontrib><creatorcontrib>Kalde, J</creatorcontrib><creatorcontrib>Averin, M</creatorcontrib><creatorcontrib>Kuuste, H</creatorcontrib><creatorcontrib>Laizans, K</creatorcontrib><creatorcontrib>Allik, V</creatorcontrib><creatorcontrib>Rauhala, T</creatorcontrib><creatorcontrib>Seppänen, H</creatorcontrib><creatorcontrib>Kiprich, S</creatorcontrib><creatorcontrib>Ukkonen, J</creatorcontrib><creatorcontrib>Haeggström, E</creatorcontrib><creatorcontrib>Kalvas, T</creatorcontrib><creatorcontrib>Tarvainen, O</creatorcontrib><creatorcontrib>Kauppinen, J</creatorcontrib><creatorcontrib>Nuottajärvi, A</creatorcontrib><creatorcontrib>Koivisto, H</creatorcontrib><title>E-sail test payload of the ESTCube-1 nanosatellite</title><title>Proceedings of the Estonian Academy of Sciences</title><description>The scientific mission of ESTCube-1, launched in May 2013, is to measure the electric solar wind sail (E-sail) force in orbit. 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| title | E-sail test payload of the ESTCube-1 nanosatellite |
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