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航空宇宙用燃料電池に係る研究の新しい展開
https://jaxa.repo.nii.ac.jp/records/6040
https://jaxa.repo.nii.ac.jp/records/604084caa702-6d07-4c3d-8c2c-ffdefb70182b
名前 / ファイル | ライセンス | アクション |
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49500056.pdf (596.9 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 航空宇宙用燃料電池に係る研究の新しい展開 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高分子電解質燃料電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 水素-酸素燃料電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 加湿 | |||||
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 | 熱真空条件 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空宇宙環境 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | polymer electrolyte fuel cell | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hydrogen oxygen fuel cell | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | humidification | |||||
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 | thermal vacuum condition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerospace environment | |||||
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 | Development of the fuel cell for aerospace applications | |||||
著者 |
曽根, 理嗣
× 曽根, 理嗣× Sone, Yoshitsugu |
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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 | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
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特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 en : JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency 巻 JAXA-SP-06-006, p. 257-260, 発行日 2006-11-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Japan Aerospace Exploration Agency (JAXA) is now developing polymer electrolyte fuel cell (PEFC) systems that can be applied to the high altitude balloon, transfer vehicle, and space craft. We designed the fuel cell system for low pressure environment where the working gases were supplied by the counter-flow method and the temperature of the system was passively controlled by the heat generated from the fuel cell stack. We assembled the system and are testing its performance under the thermal vacuum conditions. Furthermore, we started the development of a fuel cell system which can be operated by the propellants for spacecraft. We tried to operate the fuel cell using Hydrazine and Nitrogen Tetra Oxide. Through our measurements, stable generation of electricity was observed using PEFC. We also tried to measure the performance of the PEFC using the propellants with additives in order to decrease the melting point of the propellants. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049500056 | |||||
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-SP-06-006 |