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: その3
https://jaxa.repo.nii.ac.jp/records/7973
https://jaxa.repo.nii.ac.jp/records/7973778a11a9-c692-481b-93cf-1a7d4b3cf851
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: その3 | |||||
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 of Lithium-Ion Battery for the Venus Climate Orbiter "PLANET-C": Third Report | |||||
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 |
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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 | ||||||
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本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙エネルギーシンポジウム en : Space Energy Symposium 巻 29, 発行日 2010-02 |
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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29回宇宙エネルギーシンポジウム(2010年2月26日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス) | |||||
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 twenty-ninth Space Energy Symposium (February 26, 2010, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In recent years, lithium-ion cells having high discharge voltage and high energy density have been studied in many countries including Japan, the United States, and France for use as power supplies for devices in space.A lithium-ion cell having rated capacity of 13.2 Ah-developed for use in a space satellite by The Furukawa Battery Co. Ltd. and the first of its kind in the world-is onboard "Hayabusa", a planet exploration spacecraft developed by the Japan Aerospace Exploration Agency (JAXA) launched in May 2003. It is returning to the earth after acquiring samples from the asteroidItokawa.Based on fundamental technologies used in the cell for "Hayabusa" and for preparation for mounting on the "Planet-C" Venus probe scheduled for launch in spring 2010, we modified various performance parameters and developed a revised 23.5 Ah class lithium-ion cell. A simulated operation test was performed in "PLANET-C" provisional operational conditions using 23.5 Ah class lithium ion battery (EM cells) made for trial preceding evaluation; the validity of adaptability to the mission. A simulated operation test confirmed that the capacity deterioration of the cells in the "PLANET-C" mission would be suppressed to within the requirement limits.Based on development results, we produced a Flight model cell and performed assessment of durability in mechanical environments, and of safety. Evaluation of durability in mechanical environments consists of random vibration testing, sinusoidal wave vibration testing, and pyrotechnic shock testing. Through these asesments, we surveyed whether the developed cel's structure can sufficiently withstand vibrations and impacts occurring during launching of "Planet-C". Furthermore, we performed overcharge testing and external short-circuit testing as safety assessment tests.Results of assessments of durability in mechanical environments have revealed no failure or abnormal heat generation of the cell in any test. No cell abnormality such as a sudden drop of cell voltage has occurred. Safety assessments have confirmed that fracture, ignition, actuation of the pressure relief valve and a sudden temperature rise did not occur in either the overcharge test or the external short-circuit test. | |||||
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: AA0064737001 |