Curriculum Vitaes
Profile Information
- Affiliation
- Professor, Institute of Space and Astronautical Science, JAXA
- Degree
- 工学博士(東京大学)
- J-GLOBAL ID
- 200901061542880861
- researchmap Member ID
- 5000019456
Research History
8-
Apr, 2022 - Present
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Feb, 2022 - Present
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Feb, 2017 - Jan, 2022
Education
1-
- 2001
Committee Memberships
2Papers
174-
Applied Thermal Engineering, 126218-126218, Mar, 2025
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Cryogenics, 131 103652-103652, Apr, 2023
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IEEE Transactions on Applied Superconductivity, 2023
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IEEE Transactions on Applied Superconductivity, 32(6) 1-5, 2022 Peer-reviewed
Misc.
170-
電気学会金属・セラミックス研究会資料, MC-16(13-40), 2016
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Fluids engineering conference ..., 2015 "0325-1"-"0325-4", Nov 7, 2015Capacitance type void fraction sensors for cryogenic fluid has been developed by our research group. The sensors are roughly categorized into three types; arc type, small-sized arc type, and asymmetric type. In this paper, the three type sensors are compared, and each sensor's merits and demerits are indicated. The arc type sensor was first developed. The sensor is simple, but S/N ration is low and influence of "temperature drift" is large. The small-sized arc type sensor was developed for the sounding rocket S310 test No.43, so the sensor was needed to make as small as possible. The sensor succeeded to measure the void fraction of the liquid nitrogen flow even under microgravity. The asymmetric type sensor was deviced to improve the measurement accuracy. Inaccuracy of the sensor between true void fraction and measured void fraction was only 3% for stratified flow, whereas that of the arc type sensor 30%.
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平成26年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2014, 2015平成26年度宇宙輸送シンポジウム(2015年1月15日-16日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000036020レポート番号: STCP-2014-020
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International Journal of Microgravity Science and Application (Web), 32(2), 2015
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大気球シンポジウム: 平成26年度 = Balloon Symposium: 2014, Nov, 2014大気球シンポジウム 平成26年度(2014年11月6-7日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県 Balloon Symposium 2014 (November 6-7, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 著者人数: 18名 資料番号: SA6000021014 レポート番号: isas14-sbs-014
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大気球シンポジウム: 平成26年度 = Balloon Symposium: 2014, Nov, 2014大気球シンポジウム 平成26年度(2014年11月6-7日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000021011レポート番号: isas14-sbs-011
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Oct, 2013Upper stages of H-IIA and H-IIB use LOX/LH2 as a propellant and achieve high performance and reliability. Utilizingthe experiences of cryogenic propellant management, the upper stage of H-IIA is now being upgraded for more efficientmass transfer. The propulsion system development is one of the most critical issues for the H-IIA Upgrade, and willsucceed CPS, Cryogenic Propulsion Stage, which is an element of the international exploration architecture for thein-space orbital transfer. Currently, CPS was scaled up to DUUS, Dual Use Upper Stage, and JAXA is now conducting acollaborative study with NASA. It is necessary to improve understanding of cryogenic propellant management to developDUUS, hence, JAXA focuses on not only vehicle development but also basic researches with universities and industries.
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平成24年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium: FY2012, Jan, 2013平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県 Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 形態: カラー図版あり 形態: PDF 著者人数: 11名 Physical characteristics: Original contains color illustrations Physical characteristics: PDF Number of authors: 11 資料番号: AA0061856027 レポート番号: STCP-2012-027
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平成24年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium: FY2012, 1-4, Jan, 2013平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県 Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 形態: カラー図版あり 形態: PDF Physical characteristics: Original contains color illustrations Physical characteristics: PDF 資料番号: AA0061856022 レポート番号: STCP-2012-022
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電気学会超電導応用電力機器研究会資料, ASC-13(22-42), 2013
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平成24年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium: FY2012, Jan, 2013平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県形態: カラー図版あり形態: PDF資料番号: AA0061856060レポート番号: STCP-2012-060
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平成24年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium: FY2012, Jan, 2013平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県形態: カラー図版あり形態: PDF著者人数: 12名資料番号: AA0061856048レポート番号: STCP-2012-048
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FSST NEWS (Forum of Superconductivity Science and Technology News), (132), 2012
Presentations
64-
The Proceedings of Mechanical Engineering Congress, Japan, 2018<p>A loading system plays a role of loading and unloading liquid hydrogen between a carrier ship and a ground storage facility in hydrogen supply chain in which hydrogen in the form of liquid phase is transported by the carrier ship from a resource-rich country to a consuming country. An emergency release system (ERS), which is one of components of the loading system, is installed in the middle of transfer pipe of the loading system, and has function of separating and plugging the pipe at an abnormality during loading so as to prevent a large amount of cryogenic fluid from scattering. We have conducted R & D study of the ERS for liquid hydrogen based on an existing one for liquid natural gas (LNG). Whole system function of the ERS including separation behavior was verified conducting a field experiment with the ERS test model and liquid hydrogen. Through several tests, the separation mechanism and behavior were verified, and also, soundness of the seal mechanism was evaluated. While, auto-ignition phenomena were observed on the separation surface of the ERS after the separation, of which causes have not been identified yet. Characteristics of dispersion behavior of hydrogen that was released at the separation could be investigated measuring distribution of temperature and hydrogen concentration around the ERS test model.</p>
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The Proceedings of Mechanical Engineering Congress, Japan, 2018<p>To improve safety regulations for fuel cell vehicles and hydrogen infrastructure, experiments of cryo-compressed hydrogen leakage diffusion were conducted. The experimental apparatus can supply 90 MPa hydrogen of various temperature conditions. Measurement items were hydrogen concentration distribution, blast pressure, flame length, and radiant heat. In addition, high speed camera observation was carried out to investigate the near-field of cryogenic hydrogen jet at supercritical pressure. The experimental apparatus can supply 90 MPa hydrogen at various temperature conditions (50 K–300 K) at a maximum flow rate of 100 kg/h. The hydrogen leakage flow rate was measured using pinhole nozzles with different outlet diameters (0.2 mm, 0.4 mm, 0.7 mm, and 1 mm). It was confirmed that the hydrogen leakage flow rate increases as the supply temperature decreases. The hydrogen concentration distribution was measured by injecting high-pressure hydrogen from the 0.2-mm pinhole for 10 min under a constant pressure/temperature condition. As the hydrogen injection temperature decreased, it was found that the hydrogen concentration increased, and an empirical formula of the 1% concentration distance for the cryogenic hydrogen system was newly presented.</p>
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日本冷凍空調学会年次大会講演論文集 Proceedings of the JSRAE Annual Conference, 2017
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The Proceedings of Mechanical Engineering Congress, Japan, 2017
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The Proceedings of Mechanical Engineering Congress, Japan, 2017<p>JAXA has constructed an experimental facility to pressurize and supply liquid hydrogen at a maximum pressure of 90 MPa to conduct experimental research on the injection of high pressure liquid hydrogen into the atmosphere. Liquid hydrogen has a property that its density greatly changes depending on pressure despite being a liquid phase. In addition, the high pressure hydrogen gas is in a supercritical state and has an intermediate property between a gas and a liquid. Therefore, it is a difficult question whether to treat the injection of high pressure liquid hydrogen as a gas phase phenomena or as a liquid phase phenomena. As a result of the experiment, it was found good to apply the liquid orifice equation to predict the discharge flow rate of high pressure liquid hydrogen.</p>
Professional Memberships
3-
Apr, 2019 - Present
Research Projects
14-
Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2024 - Mar, 2027
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科学研究費助成事業, 日本学術振興会, Apr, 2023 - Mar, 2027
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科学研究費助成事業, 日本学術振興会, Apr, 2020 - Mar, 2023
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2019 - Mar, 2022
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2015 - Mar, 2018