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Development of Oxygen Generation Demonstration on JEM (KIBO) for Manned Space Exploration

https://jaxa.repo.nii.ac.jp/records/39555
https://jaxa.repo.nii.ac.jp/records/39555
2ff1a117-087e-405f-a09a-7f4648a862c4
Item type 会議発表論文 / Conference Paper(1)
公開日 2015-09-24
タイトル
タイトル Development of Oxygen Generation Demonstration on JEM (KIBO) for Manned Space Exploration
言語 en
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_5794
資源タイプ conference paper
アクセス権
アクセス権 metadata only access
アクセス権URI http://purl.org/coar/access_right/c_14cb
著者 Sakurai, Masato

× Sakurai, Masato

en Sakurai, Masato

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Shima, Asuka

× Shima, Asuka

en Shima, Asuka

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Sone, Yoshitsugu

× Sone, Yoshitsugu

en Sone, Yoshitsugu

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Ohnishi, Mitsuru

× Ohnishi, Mitsuru

en Ohnishi, Mitsuru

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Tachihara, Satoru

× Tachihara, Satoru

en Tachihara, Satoru

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Ito, Tsuyoshi

× Ito, Tsuyoshi

en Ito, Tsuyoshi

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著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
出版者(英)
出版者 American Institute of Aeronautics and Astronautics (AIAA)
書誌情報 発行日 2014-07
会議概要(会議名, 開催地, 会期, 主催者等)(英)
内容記述タイプ Other
内容記述 44th International Conference on Environmental Systems(July 13-17, 2014.), Tucson, Arizona, United States.
抄録(英)
内容記述タイプ Other
内容記述 To support long-duration manned space missions beyond Earth orbit, recycling life support systems will be necessary to reduce the mass of consumables required. Such systems will also have to be lightweight, compact and have low power consumption1). The Japan Aerospace Exploration Agency (JAXA) is therefore developing life support technologies2,3) for future manned space missions such as water purification, CO2 reduction and oxygen generation4,5). JAXA is currently studying an air revitalization system for an on-orbit demonstration on the International Space Station (ISS) early in the extended ISS operation period (2015–2020) to support proposed post-ISS missions such as manned lunar or asteroid exploration and an Earth-Moon Lagrange point (EML1) space station. The air and water re- vitalization subsystems of this demonstrator will be transported to the ISS separately by H- II Transfer Vehicle (HTV). Regenerative functions include oxygen recovery from carbon dioxide using a combination of CO2 reduction by the Sabatier process and O2 generation by electrolysis. Water electrolysis is a key technology because the hydrogen it produces is used for CO2 reduction and the oxygen is essential for human respiration. A simple method for obtaining dry oxygen from electrolysis is also important. This paper presents the air re- vitalization system for the demonstrator and gives details of water electrolysis in microgravity. In this paper, we investigate SPE (solid polymer electrolyte) water electrolysis and discuss the ‘Cathode Feed’ operation of an electrolyzer. Although water is usually supplied to the anode side of ground-based electrolysis cells (anode feed), we adopt cathode feed to obtain dry oxygen. The performance of the cathode feed cell can achieve its design target by flushing the gas bubbles that adhere to the electrodes.
資料番号
内容記述タイプ Other
内容記述 資料番号: PA1510097000
レポート番号
内容記述タイプ Other
内容記述 レポート番号: ICES-2014-125
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