WEKO3
アイテム
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科学衛星PLANET-Cリチウムイオン電池の開発
https://jaxa.repo.nii.ac.jp/records/8016
https://jaxa.repo.nii.ac.jp/records/80162fb3b098-4dce-4852-ab89-baf0cb46c11c
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 | 科学衛星PLANET-C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 | リチウムイオン電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機給電 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 蓄電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙技術実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | PLANET-C | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 金星探査機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙探査 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 金星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 加速寿命試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エネルギー密度 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lithium ion battery | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft power supply | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | storage battery | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space technology experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | PLANET-C | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Venus Climate Orbiter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space exploration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Venus | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | accelerated life test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | energy density | |||||
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 lithium-ion battery for the Venus Climate Orbiter PLANET-C | |||||
著者 |
大登, 裕樹
× 大登, 裕樹× 大平, 賢治× 山本, 真裕× 江黒, 高志× 豊田, 裕之× 鵜野, 将年× 廣瀬, 和之× 田島, 道夫× Oto, Hiroki× Ohira, Kenji× Yamamoto, Masahiro× Eguro, Takashi× Toyota, Hiroyuki× Uno, Masatoshi× Hirose, Kazuyuki× Tajima, Michio |
|||||
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 宇宙科学研究本部 | ||||||
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 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
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(英) | ||||||
en | ||||||
Furukawa Battery Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Furukawa Battery Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Furukawa Battery Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Furukawa Battery Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) Institute of Space and Astronautical Science (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) Institute of Space and Astronautical Science (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) Institute of Space and Astronautical Science (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) Institute of Space and Astronautical Science (ISAS) | ||||||
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27回宇宙エネルギーシンポジウム 平成19年度 en : The Twenty-seventh Space Energy Symposium p. 11-15, 発行日 2008-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Li-ion batteries, which have the advantage of high discharge voltage and high energy-to-weight ratios, have been studied energetically in recent years aiming at space applications in many countries such as Japan, the U.S. and France. Japan's asteroid explorer Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft), which was launched in May 2003 and is on its way to the Earth hopefully with some samples collected at the asteroid ITOKAWA, is the world's first spacecraft powered by a Li-ion battery, from The Furukawa Battery Corp. The battery consists of 11 prismatic 13.2 Ah battery cells connected in series and has a specific energy of more than 85 Wh/kg. The bus voltage varies from 32.5 to 47.5 V during the battery mode according to the state of charge of the battery. On the basis of the battery technology for 'Hayabusa', we started developing the Li-ion battery for the Venus Climate Orbiter 'PLANET-C' in 2002. Since a further improvement in the mass advantage was requested for the mission, the enlargement of the capacity and the increase of the energy density were examined through the surface modification of an anode active material and the improvement of the separator. As a result, a 23.5 Ah class prismatic Li-ion battery of high energy density was made for trial purposes by 2004. We performed a life test keeping the battery fully charged under the float charge condition, and found that their aged deterioration was reduced by half from the battery for 'Hayabusa'. This aged deterioration test started in 2005 followed by a float charge test and a cycle life test. We also performed a test that simulated the planned charge and discharge operations for the 'PLANET-C' mission. The results allowed us to confirm that the capacity deterioration simulation used in designing the battery was valid. Currently we are investigating the most appropriate operational pattern of the battery that controls the state of charge according to the length of the eclipses keeping the deterioration minimum. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063965003 |