タイトル | Development of Boiling and Two-Phase Flow Experiments on Board ISS: Condensation Section |
DOI | info:doi/10.15011/ijmsa.33.330103 |
著者(日) | 今井, 良二; 鈴木, 康一; 川崎, 春夫; 大田, 治彦; 新本, 康久; 浅野, 等; 河南, 治; 藤井, 清澄; 松本, 聡; 栗本, 卓; 高岡, 秀充; 坂本, 道人; 宇宿, 功史郎; 澤田, 健一郎 |
著者(英) | Imai, Ryoji; Suzuki, Koichi; Kawasaki, Haruo; Ohta, Haruhiko; Shinmoto, Yasuhisa; Asano, Hitoshi; Kawanami, Osamu; Fujii, Kiyosumi; Matsumoto, Satoshi; Kurimoto, Takashi; Takaoka, Hidemitsu; Sakamoto, Michito; Usuku, Koshiro; Sawada, Kenichiro |
著者所属(日) | 室蘭工業大学; 山口東京理科大学; 宇宙航空研究開発機構(JAXA); 九州大学; 九州大学; 神戸大学; 兵庫県立大学; 奈良先端科学技術大学院大学; 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA) |
著者所属(英) | Muroran Institute of Technology; Tokyo University of Science, Yamaguchi; Japan Aerospace Exploration Agency (JAXA); Kyushu University; Kyushu University; Kobe University; University of Hyogo; Nara Institute of Science and Technology; Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA) |
発行日 | 2016-01-31 |
発行機関など | Japan Society of Microgravity Application (JASMA) 日本マイクログラビティ応用学会(JASMA) |
刊行物名 | International Journal of Microgravity Science and Application (IJMSA) |
巻 | 33 |
号 | 1 |
開始ページ | 330103-1 |
終了ページ | 330103-5 |
刊行年月日 | 2016-01-31 |
言語 | eng |
抄録 | Thermal design and evaluation test for condenser system was conducted for the planned ISS experiments on two-phase boiling flow promoted by JAXA. Here perfluorohexane is planned to be used as a working fluid. In this condenser, eight rectangular copper tubes where circular channel of 6mm in diameter was installed on a flat type cold plate; same one which had be operated as thermal control system of on-orbit experimental modules. Arithmetic thermal model of condenser was established considering tube wall conductivity, heat transfer coefficient on condensation and cooling water flow. Specification of the condenser was determined for 400 W of the maximum heat transport requirements through the analysis by this arithmetic model. Evaluation tests using BBM and EM were conducted to verify thermal performance of condenser. In the BBM test FC72 was used as a working fluid. System requirement for condenser; that is, liquid subcooling at outlet is 10 K and more in consideration of suction performance of circular pump was proved to be satisfied. |
内容記述 | Physical characteristics: Original contains color illustrations 形態: カラー図版あり |
キーワード | Condenser; Condensation; Boiling flow; Heat transfer coefficient; Arithmetic thermal model; Evaluation test |
資料種別 | Journal Article |
NASA分類 | Space Processing |
ISSN | 0915-3616 |
NCID | AN10537663 |
SHI-NO | AA1540520000 |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/559307 |
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