WEKO3
アイテム
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金星探査機「あかつき」搭載バッテリセルの開発と運用
https://jaxa.repo.nii.ac.jp/records/7953
https://jaxa.repo.nii.ac.jp/records/79533c1290c9-c19d-4072-b4a5-2ce311d1a2e9
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 | 金星探査機「あかつき」搭載バッテリセルの開発と運用 | |||||
言語 | ||||||
言語 | jpn | |||||
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 and Operation of Battery for the Venus Climate Orbiter "AKATSUKI" | |||||
著者 |
大登, 裕樹
× 大登, 裕樹× 大平, 賢治× 山本, 真裕× 井奈福, 浩之× 豊田, 裕之× 鵜野, 将年× 廣瀬, 和之× 田島, 道夫× Ooto, Hiroki× Ohira, Kenji× Yamamoto, Masahiro× Inafuku, Hiroyuki× Toyota, Hiroyuki× Uno, Masatoshi× Hirose, Kazuyuki× Tajima, Michio |
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著者所属 | ||||||
古河電池 | ||||||
著者所属 | ||||||
古河電池 | ||||||
著者所属 | ||||||
古河電池 | ||||||
著者所属 | ||||||
古河電池 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Furukawa Battery | ||||||
著者所属(英) | ||||||
en | ||||||
Furukawa Battery | ||||||
著者所属(英) | ||||||
en | ||||||
Furukawa Battery | ||||||
著者所属(英) | ||||||
en | ||||||
Furukawa Battery | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
第30回宇宙エネルギーシンポジウム en : 30th ISAS Space Energy Symposium 発行日 2011-05-17 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第30回宇宙エネルギーシンポジウム(2011年2月25日, 宇宙航空研究開発機構宇宙科学研究所相模原キャンパス), 相模原市, 神奈川県 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The thirtieth Space Energy Symposium (February 25, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Li-ion battery, which has the advantage of high energy density, is coming into space usage in recent years. Furukawa Battery Co. Ltd. developed world's first Li-ion batteries for the asteroid explorer "HAYABUSA" of JAXA, which was launched in 2003. The batteries had rated capacity of 13.2 Ah, and continued to function normally for 3.5 years in space. Based on the fundamental technologies of these batteries, we developed 23.5-Ah Li-ion batteries for the Venus probe "PLANET-C", energy density and life performance of which were improved according to the mission requirement.The operational period of the batteries for PLANET-C can be divided into three phases; the ground storage of 1.5 years, the transfer to Venus of up to 2.5 years, and observation on the Venus orbit of over 2 years. During the batteries are stored on the ground, they are in a open-circuit state to prevent from capacity deterioration. On the transfer trajectory to Venus, the batteries retain the minimum voltage that is required for the safe-hold operation, because there is no eclipse. After Venus orbit insertion, a charge/discharge cycle operation starts.The spacecraft was successfully launched in May, 2010 and named "Akatsuki". The battery has functioned as expected in the launch operation, eclipse periods, and the Venus orbit insertion operation so far. The degradation trend of the onboard battery agreed well with that of the monitor battery on the ground and the prediction by a test using PM batteries.After the Venus orbit insertion failed last year, the spacecraft entered a new trajectory to reach at Venus six years later. Because the operational period will be much longer than originally planned, we are considering a new operational plan for the batteries to sustain as much capacity as possible. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324356 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0065107002 |