WEKO3
アイテム
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低温下での保存を可能とする電気2重層バッテリの性能評価とミッションへの適用
https://jaxa.repo.nii.ac.jp/records/11577
https://jaxa.repo.nii.ac.jp/records/115777cf8aaf2-0469-4609-867a-c9e3b1c6b3e8
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 低温下での保存を可能とする電気2重層バッテリの性能評価とミッションへの適用 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | コンデンサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電気2重層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空宇宙環境 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | はやぶさ宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 惑星探査 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MINERVAローバ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低温環境 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星ミッション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | capacitor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electrical double layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerospace environment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hayabusa spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | planetary exploration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MINERVA rover | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar cell | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low temperature environment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | asteroid mission | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development of electrical double-layer capacitor and its application to space mission | |||||
著者 |
吉光, 徹雄
× 吉光, 徹雄× 足立, 忠司× 齋藤, 浩明× 神保, 敏一× 小山, 章喜× Yoshimitsu, Tetsuo× Adachi, Tadashi× Saito, Hiroaki× Jinpo, Shunichi× Oyama, Akiyoshi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
アイ・エイチ・アイ・エアロスペース | ||||||
著者所属 | ||||||
アイ・エイチ・アイ・エアロスペース | ||||||
著者所属 | ||||||
エルナー | ||||||
著者所属 | ||||||
エルナー | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
ELNA Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
ELNA Co. Ltd. | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第4回宇宙科学シンポジウム en : Proceedings of the 4th Space Science Symposium p. 581-584, 発行日 2004-08 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Institute of Space and Astronautical Science has launched the asteroid explorer, HAYABUSA on May 2003. HAYABUSA includes the world-first asteroid rover MINERVA which will explore the asteroid surface in 2005. MINERVA needs a battery because instantaneous power generation by solar cells is insufficient for the surface exploration and data transmission tasks such as image acquisition by the onboard cameras, movement by the onboard actuator, and communication with the mother spacecraft. The night semisphere of the asteroid will be a very cold environment with the temperature lower than minus 100 C. The rover is too small to keep the inside temperature high enough for the typical batteries to be saved. Also the temperature in the day semisphere will be hotter than 100 C. Thus the onboard battery needs the availability of wide temperature range. The rover adopts the electric double-layer capacitor as the onboard electric power storage device, which can be saved under the very cold environment. The electrolytic fluid of the capacitor was tuned considering the environment of the asteroid, which enables the degradation under the very hot temperature as small as possible. So the rover is provided the ability to pass the night and the life with a couple asteroid days. This paper reports the developed electric double-layer capacitor of MINERVA asteroid rover. The energy density of the electric double-layer capacitor is smaller than the typical primary or secondary batteries under the current technical status. But it will be improved in the near future and installation to another space mission with severe temperature demand will be possible. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047899141 |