Storage of a lithium-ion secondary battery under micro-gravity conditions
| dc.contributor.author | Sone, Yoshitsugu | en |
| dc.contributor.author | Ooto, Hiroki | en |
| dc.contributor.author | Yamamoto, Masahiro | en |
| dc.contributor.author | Eguro, Takashi | en |
| dc.contributor.author | Sakai, Shigeru | en |
| dc.contributor.author | Yoshida, Teiji | en |
| dc.contributor.author | Takahashi, Keiji | en |
| dc.contributor.author | Uno, Masatoshi | en |
| dc.contributor.author | Hirose, Kazuyuki | en |
| dc.contributor.author | Tajima, Michio | en |
| dc.contributor.author | Kawaguchi, Jun'ichiro | en |
| dc.date.accessioned | 2025-12-29T17:40:38Z | |
| dc.date.available | 2025-12-29T17:40:38Z | |
| dc.date.issued | 2008-06-15 | en |
| dc.description.abstract | 'HAYABUSA' is a Japanese inter-planetary spacecraft built for the exploration of an asteroid named 'ITOKAWA.' The spacecraft is powered by a 13.2 Ah lithium-ion secondary battery. To realize maximum performance of the battery for long flight operation, the state-of-charge (SOC) of the battery was maintained at ca. 65% during storage, in case it is required for a loss of attitude control. The capacity of the battery was measured during flight operations. Along with the operation in orbit, a ground-test battery was discharged, and both results showed a good agreement. This result confirmed that the performance of the lithium-ion secondary battery stored under micro-gravity conditions is predictable using a ground-test battery. | en |
| dc.description.status | Peer-reviewed | en |
| dc.format.extent | 6 | en |
| dc.identifier.issn | 0378-7753 | en |
| dc.identifier.other | ORCID:/0000-0001-8196-5194/work/163624198 | en |
| dc.identifier.scopus | 43049165762 | en |
| dc.identifier.uri | https://hdl.handle.net/1885/733797327 | |
| dc.language.iso | en | en |
| dc.source | Journal of Power Sources | en |
| dc.subject | Aerospace | en |
| dc.subject | In-orbit | en |
| dc.subject | Lithium-ion secondary cell | en |
| dc.subject | Micro-gravity | en |
| dc.subject | Satellite | en |
| dc.subject | Spacecraft | en |
| dc.title | Storage of a lithium-ion secondary battery under micro-gravity conditions | en |
| dc.type | Journal article | en |
| dspace.entity.type | Publication | en |
| local.bibliographicCitation.lastpage | 154 | en |
| local.bibliographicCitation.startpage | 149 | en |
| local.contributor.affiliation | Sone, Yoshitsugu; Japan Aerospace Exploration Agency | en |
| local.contributor.affiliation | Ooto, Hiroki; The Furukawa Battery CO, LTD | en |
| local.contributor.affiliation | Yamamoto, Masahiro; The Furukawa Battery CO, LTD | en |
| local.contributor.affiliation | Eguro, Takashi; The Furukawa Battery CO, LTD | en |
| local.contributor.affiliation | Sakai, Shigeru; The Furukawa Battery CO, LTD | en |
| local.contributor.affiliation | Yoshida, Teiji; NEC Corporation | en |
| local.contributor.affiliation | Takahashi, Keiji; Japan Aerospace Exploration Agency | en |
| local.contributor.affiliation | Uno, Masatoshi; Japan Aerospace Exploration Agency | en |
| local.contributor.affiliation | Hirose, Kazuyuki; Japan Aerospace Exploration Agency | en |
| local.contributor.affiliation | Tajima, Michio; Japan Aerospace Exploration Agency | en |
| local.contributor.affiliation | Kawaguchi, Jun'ichiro; Japan Aerospace Exploration Agency | en |
| local.identifier.citationvolume | 181 | en |
| local.identifier.doi | 10.1016/j.jpowsour.2008.02.060 | en |
| local.identifier.pure | 6beeb270-5e30-446f-9526-7e8847dc5198 | en |
| local.identifier.url | https://www.scopus.com/pages/publications/43049165762 | en |
| local.type.status | Published | en |