WEKO3
アイテム
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M-Vロケット第3段TVCアクチュエータ駆動用高率放電リチウムイオンバッテリ
https://jaxa.repo.nii.ac.jp/records/8090
https://jaxa.repo.nii.ac.jp/records/8090b19d87d7-6c4a-428f-9661-b08620aef550
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 | M-Vロケット第3段TVCアクチュエータ駆動用高率放電リチウムイオンバッテリ | |||||
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 | 推力方向制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 可動ノズル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アクチュエータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電流密度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エネルギー密度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 銀亜鉛電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 環境試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動試験 | |||||
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 | thrust vector control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | movable nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | actuator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | current density | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | energy density | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | silver zinc battery | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | environmental test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibration test | |||||
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 Li-ion battery for the 3rd stage TVC system of the M-V launch vehicle | |||||
著者 |
森田, 泰弘
× 森田, 泰弘× 曽根, 理嗣× 安田, 誠一× 佐藤, 豊× 長谷川, 和雄× 加藤, 弘一郎× 中野, 隆行× Morita, Yasuhiro× Sone, Yoshitsugu× Yasuda, Seiichi× Sato, Yutaka× Hasegawa, Kazuo× Kato, Koichiro× Nakano, Takayuki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
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 | ||||||
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(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
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 | ||||||
IHI Aerospace Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace 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24回宇宙エネルギーシンポジウム 平成16年度 en : The Twenty-fourth Space Energy Symposium March 7, 2005 p. 17-21, 発行日 2005-06 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The TVC (Thrust Vector Control) system for the 3rd stage of the M-V launch vehicle performs thrust direction control by driving a movable nozzle with two electric actuators, and uses a Silver-Zinc battery to supply 28 V electric power to them. A high-power density battery for launch vehicle did not exist except the Silver-Zinc battery when the M-V TVC system was developed. Therefore, Silver-Zinc battery was adopted, although it has drawbacks of its short storage life and charge/discharge cycle life. After four launches of M-V, this battery system needs to be reconsidered, because of above demerits. The new battery requirements are as follows, (1) Long storage and cycle life, (2) Low cost, (3) Small size and light weight. We selected the lithium ion battery for HEV (Hybrid Electric Vehicle), that can satisfy our requirements. This battery has the following key advantages, (a) High discharge rate, (b) Long life, (c) Low cost, (d) Stabilized Quality, and (e) High safety design. To apply the lithium ion battery for HEV to M-V launch vehicle the following items have been verified. (1) Electrical compatibility with the TVC system of the M-V launch vehicle, (2) Environmental resistance, (3) Space level quality assurance. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049120004 |