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  1. シンポジウム・研究会
  2. 宇宙科学シンポジウム
  3. 第4回
  1. コンテンツタイプ
  2. 会議発表論文/会議発表用資料 (Conference Paper/Presentation)

低温下での保存を可能とする電気2重層バッテリの性能評価とミッションへの適用

https://jaxa.repo.nii.ac.jp/records/11577
https://jaxa.repo.nii.ac.jp/records/11577
7cf8aaf2-0469-4609-867a-c9e3b1c6b3e8
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 低温下での保存を可能とする電気2重層バッテリの性能評価とミッションへの適用
言語
言語 jpn
キーワード
主題Scheme Other
主題 コンデンサ
キーワード
主題Scheme Other
主題 電気2重層
キーワード
主題Scheme Other
主題 航空宇宙環境
キーワード
主題Scheme Other
主題 はやぶさ宇宙機
キーワード
主題Scheme Other
主題 惑星探査
キーワード
主題Scheme Other
主題 MINERVAローバ
キーワード
主題Scheme Other
主題 太陽電池
キーワード
主題Scheme Other
主題 低温環境
キーワード
主題Scheme Other
主題 小惑星ミッション
キーワード
言語 en
主題Scheme Other
主題 capacitor
キーワード
言語 en
主題Scheme Other
主題 electrical double layer
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 Hayabusa spacecraft
キーワード
言語 en
主題Scheme Other
主題 planetary exploration
キーワード
言語 en
主題Scheme Other
主題 MINERVA rover
キーワード
言語 en
主題Scheme Other
主題 solar cell
キーワード
言語 en
主題Scheme Other
主題 low temperature environment
キーワード
言語 en
主題Scheme Other
主題 asteroid mission
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 electrical double-layer capacitor and its application to space mission
著者 吉光, 徹雄

× 吉光, 徹雄

WEKO 102202

吉光, 徹雄

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足立, 忠司

× 足立, 忠司

WEKO 102203

足立, 忠司

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齋藤, 浩明

× 齋藤, 浩明

WEKO 102204

齋藤, 浩明

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神保, 敏一

× 神保, 敏一

WEKO 102205

神保, 敏一

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小山, 章喜

× 小山, 章喜

WEKO 102206

小山, 章喜

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Yoshimitsu, Tetsuo

× Yoshimitsu, Tetsuo

WEKO 102207

en Yoshimitsu, Tetsuo

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Adachi, Tadashi

× Adachi, Tadashi

WEKO 102208

en Adachi, Tadashi

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Saito, Hiroaki

× Saito, Hiroaki

WEKO 102209

en Saito, Hiroaki

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Jinpo, Shunichi

× Jinpo, Shunichi

WEKO 102210

en Jinpo, Shunichi

Search repository
Oyama, Akiyoshi

× Oyama, Akiyoshi

WEKO 102211

en Oyama, Akiyoshi

Search repository
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
アイ・エイチ・アイ・エアロスペース
著者所属
アイ・エイチ・アイ・エアロスペース
著者所属
エルナー
著者所属
エルナー
著者所属(英)
en
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
著者所属(英)
en
IHI Aerospace Co. Ltd.
著者所属(英)
en
IHI Aerospace Co. Ltd.
著者所属(英)
en
ELNA Co. Ltd.
著者所属(英)
en
ELNA Co. Ltd.
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4回宇宙科学シンポジウム
en : Proceedings of the 4th Space Science Symposium

p. 581-584, 発行日 2004-08
抄録(英)
内容記述タイプ Other
内容記述 The Institute of Space and Astronautical Science has launched the asteroid explorer, HAYABUSA on May 2003. HAYABUSA includes the world-first asteroid rover MINERVA which will explore the asteroid surface in 2005. MINERVA needs a battery because instantaneous power generation by solar cells is insufficient for the surface exploration and data transmission tasks such as image acquisition by the onboard cameras, movement by the onboard actuator, and communication with the mother spacecraft. The night semisphere of the asteroid will be a very cold environment with the temperature lower than minus 100 C. The rover is too small to keep the inside temperature high enough for the typical batteries to be saved. Also the temperature in the day semisphere will be hotter than 100 C. Thus the onboard battery needs the availability of wide temperature range. The rover adopts the electric double-layer capacitor as the onboard electric power storage device, which can be saved under the very cold environment. The electrolytic fluid of the capacitor was tuned considering the environment of the asteroid, which enables the degradation under the very hot temperature as small as possible. So the rover is provided the ability to pass the night and the life with a couple asteroid days. This paper reports the developed electric double-layer capacitor of MINERVA asteroid rover. The energy density of the electric double-layer capacitor is smaller than the typical primary or secondary batteries under the current technical status. But it will be improved in the near future and installation to another space mission with severe temperature demand will be possible.
資料番号
内容記述タイプ Other
内容記述 資料番号: AA0047899141
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