@inproceedings{oai:jaxa.repo.nii.ac.jp:00038704,
 author = {宮田, 純弥 and 寺本, 正明 and 岡田, 治 and 井崎, 博和 and 野々内, 保 and 花井, 伸彰 and 清原, 八里 and 桜井, 誠人 and Miyata, Junya and Teramoto, Masaaki and Okada, Osamu and Izaki, Hirokazu and Nonouchi, Tamotsu and Hanai, Nobuaki and Kiyohara, Yasato and Sakurai, Masato},
 book = {第58回宇宙科学技術連合講演会講演集, Proceedings of 58th Space Sciences and Technology Conference},
 month = {Nov},
 note = {第58回宇宙科学技術連合講演会（2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県, "In the application of membrane separation to the removal of CO2 in ISS and space suits, membranes with extremely high CO2/O2 and CO2/N2 selectivities at room temperature and low CO2 partial pressures are indispensable for minimizing O2 and N2 losses. In this study, we developed CO2 facilitated transport membranes consisting of hygroscopic gel and CO2 carrier. An additive was added to some membranes, which decreased N2 and O2 permeances remarkably with little change in CO2 permeance, resulting in very high CO2/N2 and CO2/O2 selectivities. Typical membrane performances are as follows. CO2 permeance: 2.71×10-5 - 5.70×10-5 mol/m2 s kPa, CO2/N2 selectivity: 5210-13700, at the CO2 partial pressure of 0.7 kPa and 26.7℃. These values are much larger than previously reported values.Feasibility studies on the CO2 separation in ISS and space suits were performed where membrane modules fabricated by incorporating developed membranes are supposed to be used. It was found that CO2 could be concentrated to higher than 96% (dry basis) by a single stage membrane separation.", 資料番号: AC1500064000, レポート番号: JSASS-2014-4392},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {CO2 膜分離法の宇宙分野への応用(2)},
 year = {2014}
}