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
5-
Feb, 2022 - Present
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Feb, 2017 - Jan, 2022
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Oct, 2003 - Jan, 2017
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2001 - 2002
Education
1-
- 2001
Papers
169-
Cryogenics, 131 103652-103652, Apr, 2023
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IEEE Transactions on Applied Superconductivity, 32(6) 1-5, 2022 Peer-reviewedThe critical heat flux in liquid hydrogen is ten times higher than that in liquid helium and is approximately half of that in liquid nitrogen. Since the resistivity of pure metal such as copper or silver at 20 K is less than one-hundredth of that at 300 K, HTS magnets immersed in liquid hydrogen are expected to satisfy the fully cyostable condition or to be stable against high resistive heat generation enough for quench detection at a practical current density. In order to examine cryostability of HTS magnets in liquid hydrogen, a pool-cooled Bi2223 magnet with a 5 T magnetic field at 20 K has been designed, fabricated and tested in liquid nitrogen prior to excitation tests in liquid hydrogen. The magnet consists of six outer double pancake coils with the inner diameter of 0.20 m and four inner double pancake coils with the outer diameter of 0.16 m. The resistive voltage to initiate thermal runaway in the coil as-sembly in liquid nitrogen was higher than 1 V that is sufficient high for quench detection.
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日本航空宇宙学会論文集, 70(4), 2022
Misc.
168-
Proceedings of Sounding Rocket Symposium 2023, Feb, 2024誤記: NAKATA, Dasuke
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日本機械学会年次大会講演論文集(CD-ROM), 2024, 2024
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 63rd, 2024
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日本冷凍空調学会論文集, 41(2), 2024
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日本航空宇宙学会年会講演会講演集(CD-ROM), 54th, 2023
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令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022, Jan, 2023令和4年度宇宙輸送シンポジウム(2023年1月12日-13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 Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 資料番号: SA6000184015 STCP-2022-015
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宇宙科学技術連合講演会講演集(CD-ROM), 66th, 2022
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令和3年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2021, Jan, 2022令和3年度宇宙輸送シンポジウム(2022年1月13日-14日. オンライン開催) Space Transportation Symposium FY2021 (January 13-14, 2022. Online Meeting) 著者人数: 12名 資料番号: SA6000173016 STCP-2021-016
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令和3年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2021, Jan, 2022令和3年度宇宙輸送シンポジウム(2022年1月13日-14日. オンライン開催) Space Transportation Symposium FY2021 (January 13-14, 2022. Online Meeting) 著者人数: 16名 資料番号: SA6000173015 STCP-2021-015
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流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM), 53rd-39th, 2021
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宇宙科学技術連合講演会講演集(CD-ROM), 65th, 2021
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Jan, 2021Space Transportation Symposium FY2020 (January 14-15, 2021. Online Meeting)
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令和元年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2019, Jan, 2020令和元年度宇宙輸送シンポジウム(2020年1月16日-17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 Symposium FY2019 (January 16-17, 2020. 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: SA6000147018 レポート番号: STCP-2019-018
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日本機械学会流体工学部門講演会講演論文集(CD-ROM), 98th, 2020
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低温工学・超電導学会講演概要集, 100th, 2020
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Jan, 2020Space Transportation Symposium FY2019 (January 16-17, 2020. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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数値流体力学シンポジウム講演論文集(CD-ROM), 34th, 2020
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低温工学・超電導学会講演概要集, 99th, 2020
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宇宙科学技術連合講演会講演集(CD-ROM), 64th, 2020
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宇宙科学技術連合講演会講演集(CD-ROM), 64th, 2020
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観測ロケットシンポジウム2019 講演集 = Proceedings of Sounding Rocket Symposium 2019, Aug, 2019第2回観測ロケットシンポジウム(2019年8月5日-6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 2nd Sounding Rocket Symposium (August 5-6, 2019. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 著者人数: 17名 資料番号: SA6000142008 レポート番号: Ⅲ-1
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観測ロケットシンポジウム2019 講演集 = Proceedings of Sounding Rocket Symposium 2019, Aug, 2019第2回観測ロケットシンポジウム(2019年8月5日-6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: SA6000142004レポート番号: Ⅰ-4
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宇宙科学技術連合講演会講演集(CD-ROM), 63rd, 2019
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日本機械学会年次大会講演論文集(CD-ROM), 2019, 2019
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 59th, 2019
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日本機械学会設計工学・システム部門講演会論文集(CD-ROM), 29th, 2019
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観測ロケットシンポジウム2018 講演集 = Proceedings of Sounding Rocket Symposium 2018, Jul, 2018第1回観測ロケットシンポジウム(2018年7月17日-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 1st Sounding Rocket Symposium (July 17-18, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 著者人数: 14名 資料番号: SA6000127002 レポート番号: Ⅰ-2
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Jan, 2018Space Transportation Symposium FY2017 (January 18-19, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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宇宙科学技術連合講演会講演集(CD-ROM), 61st, 2017
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 57th, 2017
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
13-
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
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, May, 2013 - Mar, 2018