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Thermal Behavior of Axially Grooved Heat Pipes aboard a Rocket
https://jaxa.repo.nii.ac.jp/records/31359
https://jaxa.repo.nii.ac.jp/records/31359642b9e58-e457-4f70-a45f-01e814b6812b
名前 / ファイル | ライセンス | アクション |
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SA0034916.pdf (1.1 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Thermal Behavior of Axially Grooved Heat Pipes aboard a Rocket | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
著者 |
MURAKAMI, Masahide
× MURAKAMI, Masahide× TADEUCHI, Ryo× HAYASHI, Tomonao× MACHIDA, Tsuneo× KATO, Seiichi× MATSUFUJI, Yukio |
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著者所属(英) | ||||||
en | ||||||
Institute of Structural Engineering, University of Tsukuba. | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Structural Engineering, University of Tsukuba. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Nippon Electric Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Nippon Electric Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Nippon Electric Co., Ltd. | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science | |||||
書誌情報 |
en : The Institute of Space and Astronautical Science report 巻 601, p. 1-19, 発行日 1982-10 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Two axially grooved heat pipes, one using ammonia as the working fluid and another using freon 11,were launched aboard S-520 sounding rockets in January 1980 and in September 1981,respectively. The former was made of aluminum and the latter of aluminum alloy. N-eicosane was employed as a phase change heat sink material for both cases. They were fixed on the rocket axis with the condenser top. The heat pipes experienced several levels of varying acceleration such as large positive during the boosting period, small negative immediately after the burnout caused by the aerodynamic drag on the rocket, zero-gravity, and again positive while the re-entry. They responded to these situations. Such responses as dryout, recovery from the dryout with partial liquid blockage in the condenser section, and resumption of normal heat pipe operation were resulted from the dynamic behavior of the working fluid. The flight data were analyzed to understand the heat pipe performance and to investigate the dependence of the liquid motion on the body force and on the surface tension. The critical Bond number which gave a boundary between surface tension dominating and body force dominating regions was found to be the order of 10^-3 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0285-6808 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA10632072 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0034916000 |