WEKO3
アイテム
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宇宙用リチウムイオン電池の開発
https://jaxa.repo.nii.ac.jp/records/8154
https://jaxa.repo.nii.ac.jp/records/8154ac6a0580-bbe9-4582-865e-08b129b0db04
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 | 宇宙用リチウムイオン電池の開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Liイオンセル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高エネルギー密度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙応用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 長寿命 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 密封封印 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱真空試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 照射試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙環境 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Li ion cell | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high energy density | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space application | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | long life | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hermetic seal | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibration test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal vacuum test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | irradiation test | |||||
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 | research and development | |||||
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 L[lc]i-ion cells for space applications | |||||
著者 |
今村, 文隆
× 今村, 文隆× 井上, 剛文× 吉田, 浩明× 水谷, 実× Imamura, Nobutaka× Inoue, Takefumi× Yoshida, Hiroaki× Mizutani, Minoru |
|||||
著者所属 | ||||||
日本電池 産業電池生産カンパニー | ||||||
著者所属 | ||||||
日本電池 産業電池生産カンパニー | ||||||
著者所属 | ||||||
日本電池 産業電池生産カンパニー | ||||||
著者所属 | ||||||
日本電池 産業電池生産カンパニー | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Storage Battery Co. Ltd. Industrial Battery Manufacturing Company | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Storage Battery Co. Ltd. Industrial Battery Manufacturing Company | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Storage Battery Co. Ltd. Industrial Battery Manufacturing Company | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Storage Battery Co. Ltd. Industrial Battery Manufacturing Company | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | The Institute of Space and Astronautical Science (ISAS) | |||||
書誌情報 |
第22回宇宙エネルギーシンポジウム 平成14年度 en : The 22nd ISAS Space Energy Symposium March 12, 2003 p. 16-20, 発行日 2003-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | High energy density Li-ion battery is expected for the next generation satellite and the other space usage. Japan Storage Battery Co., Ltd. (JSB) has developed two types of large capacity Li-ion cells through cooperation with Mitsubishi Electric Corporation (MELCO). One is satellite type (50, 100 and 175 Ah) for long life applications and the other is rocket type (55, 110 and 190 Ah) for high energy applications. The energy density of the cells are 136 Wh/kg to 164 Wh/kg. They correspond to the 1.5 to 2.0 times of Ni-H2 cell. The cells have completely sealed structure achieved with ceramic hermetic seal in order to endure the space environment. It has been confirmed that the cells performance satisfies space application requirements by many tests and analysis as follows: For environmental characteristics evaluation, various environmental tests such as vibration tests, thermal vacuum tests, irradiation tests and so on have been performed for the cells. It is found that the cells satisfy general environmental requirements of space applications. 100 Ah Li-ion cells have been qualified for space applications by MELCO. For cell life evaluation, the calendar life test and the cycle life test have been performed in matrix of temperature, state of charge (SOC), and depth of discharge (DOD). As the results, experimental equations for capacity fading has been found out. The equations have been verified by comparing capacity estimation curve and test data. By using the experimental equations, it was tried to calculate capacity fading for general geostationary orbit (GEO) and low earth orbit (LEO) satellites applications. It was confirmed that the estimation suggested the 100 Ah Li-ion cells satisfied requirements for their use in general satellites. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0045915004 |