Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in Space
The lithium-ion secondary batteries have been widely used for the space programs, today. Among them, REIMEI was one of the first satellites using lithium-ion secondary battery. In 2005, the satellite was launched, and injected into the low earth polar orbit. Eleven years has passed since the launch...
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EDP Sciences
2017-01-01
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| Series: | E3S Web of Conferences |
| Online Access: | https://doi.org/10.1051/e3sconf/20171607005 |
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doaj-86a69ab9d64f4b6cbff76b925410da532021-02-02T07:42:22ZengEDP SciencesE3S Web of Conferences2267-12422017-01-01160700510.1051/e3sconf/20171607005e3sconf_espc2017_07005Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in SpaceSone YoshitsuguWatanabe Hiromi0Tanaka Kohei1Mendoza-Hernandez Omar Samuel2Fukuda SeisukeItagaki Masayuki3Ogawa Keita4Asamura KazushiYamazaki Atsushi5Nagamatsu Hiroyuki6Fukushima YosukeSaito HirofumiThe University of Tokyo, Saito Lab.The Graduate University of Advanced Studies (SOKENDAI)Japan Aerospace Exploration AgencyTokyo University of ScienceAdvanced Engineering Services Co. Ltd.Japan Aerospace Exploration AgencyJapan Aerospace Exploration AgencyThe lithium-ion secondary batteries have been widely used for the space programs, today. Among them, REIMEI was one of the first satellites using lithium-ion secondary battery. In 2005, the satellite was launched, and injected into the low earth polar orbit. Eleven years has passed since the launch and over 60,000 cycles of charge and discharge was experienced in space. The lithium-ion secondary cell of the REIMEI battery was designed using spinel manganese oxide type material for the positive electrode, and the graphitized type carbon for the negative electrode. The cell case was made of aluminium laminated film and the structure was reinforced by the epoxy resin and aluminium housing. After the operation of eleven years, the cells still maintain the appropriate uniform balance and operative. In order to identify the internal condition of the battery/cell, we calculated the ac impedance by the pulse duration to the on-board battery.https://doi.org/10.1051/e3sconf/20171607005 |
| collection |
DOAJ |
| language |
English |
| format |
Article |
| sources |
DOAJ |
| author |
Sone Yoshitsugu Watanabe Hiromi Tanaka Kohei Mendoza-Hernandez Omar Samuel Fukuda Seisuke Itagaki Masayuki Ogawa Keita Asamura Kazushi Yamazaki Atsushi Nagamatsu Hiroyuki Fukushima Yosuke Saito Hirofumi |
| spellingShingle |
Sone Yoshitsugu Watanabe Hiromi Tanaka Kohei Mendoza-Hernandez Omar Samuel Fukuda Seisuke Itagaki Masayuki Ogawa Keita Asamura Kazushi Yamazaki Atsushi Nagamatsu Hiroyuki Fukushima Yosuke Saito Hirofumi Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in Space E3S Web of Conferences |
| author_facet |
Sone Yoshitsugu Watanabe Hiromi Tanaka Kohei Mendoza-Hernandez Omar Samuel Fukuda Seisuke Itagaki Masayuki Ogawa Keita Asamura Kazushi Yamazaki Atsushi Nagamatsu Hiroyuki Fukushima Yosuke Saito Hirofumi |
| author_sort |
Sone Yoshitsugu |
| title |
Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in Space |
| title_short |
Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in Space |
| title_full |
Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in Space |
| title_fullStr |
Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in Space |
| title_full_unstemmed |
Internal Impedance of the Lithium-Ion Secondary Cells Used for Reimei Satellite after the Eleven Years Operation in Space |
| title_sort |
internal impedance of the lithium-ion secondary cells used for reimei satellite after the eleven years operation in space |
| publisher |
EDP Sciences |
| series |
E3S Web of Conferences |
| issn |
2267-1242 |
| publishDate |
2017-01-01 |
| description |
The lithium-ion secondary batteries have been widely used for the space programs, today. Among them, REIMEI was one of the first satellites using lithium-ion secondary battery. In 2005, the satellite was launched, and injected into the low earth polar orbit. Eleven years has passed since the launch and over 60,000 cycles of charge and discharge was experienced in space.
The lithium-ion secondary cell of the REIMEI battery was designed using spinel manganese oxide type material for the positive electrode, and the graphitized type carbon for the negative electrode. The cell case was made of aluminium laminated film and the structure was reinforced by the epoxy resin and aluminium housing. After the operation of eleven years, the cells still maintain the appropriate uniform balance and operative. In order to identify the internal condition of the battery/cell, we calculated the ac impedance by the pulse duration to the on-board battery. |
| url |
https://doi.org/10.1051/e3sconf/20171607005 |
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