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宇宙用アンモニア小型流体駆動源の初期開発検討
https://jaxa.repo.nii.ac.jp/records/6261
https://jaxa.repo.nii.ac.jp/records/6261b082ae2e-aa60-4e31-9d12-cf68076ab8d0
名前 / ファイル | ライセンス | アクション |
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49054005.pdf (1.2 MB)
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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 | 宇宙用アンモニア小型流体駆動源の初期開発検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱制御システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アンモニア | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝達 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | メカニカルポンプ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 発熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 作動流体 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal control system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ammonia | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat transfer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mechanical pump | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat generation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | working fluid | |||||
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 | Preliminary study on development of a small-sized mechanical pump | |||||
著者 |
矢部, 高弘
× 矢部, 高弘× 川崎, 春夫× Yabe, Takahiro× Kawasaki, Haruo |
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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 | ||||||
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16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems 巻 JAXA-SP-05-008, p. 21-24, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This report describes the development of a small-sized mechanical pump. The pump can be used in thermal control systems, such as Mechanical Pumped Loops (MPL) of spacecraft. This pump has following three features. (1) Ammonia used as working fluid. (2) Small sized design for spacecraft. (3) Axial type motor used for driving gear. The trochoid gear miniaturized the pump with the external diameter of 48 mm, the thickness of 19 mm and weight of 150 g. As a result of the performance test, 0.5 L/min flow rate, 45 kPa of total pressure and 2 MPa withstand pressure were achieved. | |||||
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: AA0049054005 | |||||
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-05-008 |