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MDS-1バスバッテリの軌道上評価
https://jaxa.repo.nii.ac.jp/records/2709
https://jaxa.repo.nii.ac.jp/records/27097e0e5e6f-c7dc-46da-8f74-fbb1612bd9e3
名前 / ファイル | ライセンス | アクション |
---|---|---|
48057018.pdf (2.0 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | MDS-1バスバッテリの軌道上評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MDS-1 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2A打上げ機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Ni-MH電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 食 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽電力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低コスト | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 放電 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MDS-1 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H-2A launch vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ni-MH battery | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | eclipse | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar power | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low cost | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electric discharge | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Orbital performance of MDS-1 Ni-MH battery | |||||
著者 |
山田, 知佐
× 山田, 知佐× 艸分, 宏昌× 桑島, 三郎× Yamada, Chisa× Kusawake, Hiroaki× Kuwajima, Saburo |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:衛星系 en : JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System 巻 JAXA-RM-04-010, p. 87-90, 発行日 2004-10-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Mission Demonstration Test Satellite-1 (MDS-1 or Tsubasa) has 2 batteries, which consist of 32 series of 20 Ah Ni-MH cells. These batteries showed good performance as the main power source of the satellite during eclipse, which solar power isn't available. The satellite, which was launched by H-2A Launch Vehicle No. 2 (H-2A F2) on February 4, 2002, has ended its one year and eight months onorbit mission, which was much longer than the scheduled mission period of a year, and acquired various data. On September 25, 2003, the command signal was sent to stop radio frequency (RF) emission from the satellite. In this paper, orbital performance of these Ni-MH batteries on MDS-1 is reported. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048057018 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RM-04-010 |