JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

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title金星探査機「あかつき」搭載バッテリセルの開発と運用
Other TitleDevelopment and Operation of Battery for the Venus Climate Orbiter "AKATSUKI"
Author(jpn)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
Author(eng)Ooto, Hiroki; Ohira, Kenji; Yamamoto, Masahiro; Inafuku, Hiroyuki; Toyota, Hiroyuki; Uno, Masatoshi; Hirose, Kazuyuki; Tajima, Michio
Author Affiliation(jpn)古河電池; 古河電池; 古河電池; 古河電池; 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS); 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS); 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS); 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)
Author Affiliation(eng)Furukawa Battery; Furukawa Battery; Furukawa Battery; Furukawa Battery; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Issue Date2011-05-17
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構宇宙科学研究所
Publication title30th ISAS Space Energy Symposium
第30回宇宙エネルギーシンポジウム
Publication date2011-05-17
Languagejpn
eng
AbstractLi-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.
DescriptionPhysical characteristics: Original contains color illustrations
Meeting Information: The thirtieth Space Energy Symposium (February 25, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan
Note: One CD-ROM
形態: カラー図版あり
会議情報: 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
形態: CD-ROM1枚
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
NCIDAN10324356
SHI-NOAA0065107002
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/18623


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