@article{oai:jaxa.repo.nii.ac.jp:00021621,
 author = {今井, 良二 and 鈴木, 康一 and 川崎, 春夫 and Hong, Chungpyo and 石塚, 博弥 and 藤井, 清澄 and 新本, 康久 and 大田, 治彦 and Imai, Ryoji and Suzuki, Koichi and Kawasaki, Haruo and Hong, Chungpyo and Ishizuka, Hiroya and Fujii, Kiyosumi and Shinmoto, Yasuhisa and Ohta, Haruhiko},
 issue = {2},
 journal = {日本マイクログラビティ応用学会誌, JASMA : Journal of the Japan Society of Microgravity Application},
 month = {},
 note = {Design of condenser planned to be installed on boiling flow experiment on ISS was conducted. In this condenser, rectangular vapor tube was installed on flat type cold plate which had experienced on-orbit experiments. Arithmetic thermal model was constructed, which considered tube wall conductivity, heat transfer coefficient on condensation and cooling water flow. Specification of condenser which can condensate vapor of 400W was determined through analysis by this arithmetic model., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: DS1440148000},
 pages = {S109--S111},
 title = {Thermal Control System for Space Experiment on Two-Phase Boiling Flow-I: Analysis and Design of Condenser},
 volume = {28},
 year = {2011}
}