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
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日本航空宇宙学会論文集, 70(4), 2022
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IEEE Transactions on Applied Superconductivity, 31(5), Aug, 2021
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International Journal of Hydrogen Energy, 46(57) 29583-29596, Aug, 2021 Peer-reviewed
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Journal of Spacecraft and Rockets, 58(5) 1-14, Jun 28, 2021 Peer-reviewed
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 46(11) 8239-8252, Feb, 2021 Peer-reviewed
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CRYOGENICS, 113, Jan, 2021 Peer-reviewed
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CRYOGENICS, 112, Dec, 2020 Peer-reviewed
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Journal of Physics: Conference Series, 1559(1), Jun 19, 2020
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 45(7) 5098-5109, Feb, 2020 Peer-reviewed
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The Proceedings of Mechanical Engineering Congress, Japan, 2020 J19101, 2020
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CRYOGENICS, 105, Jan, 2020 Peer-reviewed
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IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY, 29(5), Aug, 2019 Peer-reviewed
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IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY, 29(5), Aug, 2019 Peer-reviewed
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Transaction of JSASS, 18 109-118, Jul, 2019 Peer-reviewed
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 44(33) 18483-18495, Jul, 2019 Peer-reviewed
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IOP Conference Series: Materials Science and Engineering, 502(1), Jun 3, 2019 Peer-reviewed
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IOP Conference Series: Materials Science and Engineering, 502(1), Jun 3, 2019 Peer-reviewed
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PROMOTE THE PROGRESS OF THE PACIFIC-BASIN REGION THROUGH SPACE INNOVATION, 166 45-57, 2019 Peer-reviewed
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AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 18 19-28, 2019 Peer-reviewed<p>Many space vehicles are powered by liquid hydrogen and liquid oxygen. Such fuel are cryogenic fluids, so they are easy to boil and become gas-liquid two phase flow. The LE-5B-3 engine has the capability of the idle mode firing same as the LE-5B-2 engine. Assessment of flow condition at the inlet of fuel turbo pump is important to operate the engine, because the fuel may flow in saturated condition under the idle mode in principle. In a two-phase flow state, void fraction is one of the most important parameters to assess the flow. Although many types of void fraction sensors were proposed, the capacitive technique has advantages to mount on the engine from the viewpoint of size, weight, toughness. In this study, plural circular electrodes capacitive void fraction sensor is developed for LE-5B-3 engines' ground firing test. The sensor was designed based on electric field analysis, and the specification was assessed prior to the ground test. The sensor was used in qualification test, and it was succeeded in achieving stable measurement and it helped to understand the fluid state during the engine operation. The sensor design technique, the assessment results and the ground test results are discussed in this paper.</p>
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JOURNAL OF SPACECRAFT AND ROCKETS, 56(1) 91-103, Jan, 2019 Peer-reviewed
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CRYOGENICS, 96 25-33, Dec, 2018 Peer-reviewed
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CRYOGENICS, 94 36-44, Sep, 2018 Peer-reviewed
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 43(37) 17928-17937, Sep, 2018 Peer-reviewed
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 43(37) 17938-17953, Sep, 2018 Peer-reviewed
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Physics of Fluids, 30(6), Jun 1, 2018 Peer-reviewed
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DNB heat flux on inner side of a vertical pipe in forced flow of liquid hydrogen and liquid nitrogenCRYOGENICS, 92 105-117, Jun, 2018 Peer-reviewed
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日本航空宇宙学会誌 = Aeronautical and space sciences Japan, 66(2) 41-46, Feb, 2018
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Advances in the Astronautical Sciences, 166 45-57, 2018
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The Proceedings of Mechanical Engineering Congress, Japan, 2018 J0120104, 2018A 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.
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 66(6) 147-152, 2018 Peer-reviewed<p>Reducing the amount of propellant for re-cooling is an important issue for the rocket propulsion system using cryogenic fuel. Immediately after the start of the engine, the liquid fuel boils and becomes two-phase flow. In the state of two-phase flow, the void fraction, which is the gas-liquid ratio, is one of the important value for flow control. For above problem, we are developing void fraction measurement system for the cryogenic fluid. These devices were attached to the S310-43 sounding rocket for the purpose of "measuring two-phase flow behavior and heat transfer characteristics during coasting flight." These devices withstood the vibration shock test of 40G and succeeded to measure the void fraction of liquid/gas nitrogen two phase flow under vacuumed and microgravity circumstance. This report explains development and experiment results of the void fraction sensor and a capacitance amplifier. </p>
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Aeronautical and Space Sciences Japan, 66(2) 41-46, 2018<p>超電導推進システムを使用する水素航空機の概念検討を行った.従来のターボファンエンジンに比べてバイパス比を向上させて低騒音化と推進効率向上を図るため,超電導モータで駆動する分散ファンを備えた推進システムを想定し,設計仕様を設定した.超電導を維持するための冷媒としては,極低温の液体水素燃料を使用することを想定した.過去の超電導発電機/モータの開発事例を参考にして諸元を設定するとともに,設計回転数と分散ファン個数を変更して,質量の変化を評価した.結果として,回転子の周速を変えずに設計回転数を上昇させることで,超電導発電機/モータの寸法と質量を大幅に低減できる可能性があることを確認した.また,分散ファンについては,超電導モータの質量を低減するために,減速機と組み合わせて設計回転数をさらに向上させる必要があることを確認した.さらに,超電導発電機/モータの出力と質量の関係を整理した.</p>
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IOP Conference Series: Materials Science and Engineering, 278(1), Dec 30, 2017 Peer-reviewed
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IOP Conference Series: Materials Science and Engineering, 278(1), Dec 30, 2017 Peer-reviewed
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INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 111 115-122, Aug, 2017 Peer-reviewed
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Aeronautical and Space Sciences Japan, 65(4) 89-95, 2017
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53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017, 2017
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The Proceedings of Mechanical Engineering Congress, Japan, 2017 J0110205, 2017
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The Proceedings of Mechanical Engineering Congress, Japan, 2017 J0110104, 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>
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IEEE Transactions on Applied Superconductivity, 26(3), Apr, 2016 Peer-reviewed
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Journal of Fluid Science and Technology, 11(2) JFST0008-JFST0008, 2016A capacitance-based void fraction sensor has been developed for the rocket or airbreathing engines, which is simple and do not disturb the flow. Typical conventional sensors usually have two concave electrodes mounted on the outer wall of the dielectric tube. They are relatively low accuracy if they have a noise shield; the maximum measurement error is over 30% in our research. The aim of this study is to improve the measurement accuracy while keeping the advantage of simplicity, mountability and non-intrusive characteristics. A theoretical formulae and electromagnetic field analysis, EFA, are used to design the sensors and are compared to an experiment using air/silicon-oil mixture flow. As the result, a newly developed asymmetrical type sensor which consists of asymmetric flat electrodes with side walls shows good performance; the inaccuracy between true void fraction and measured void fraction is 6% for the stratified flow.
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The Proceedings of the Thermal Engineering Conference, 2016 C113, 2016<p>The payload capacity of launch vehicles must be increased in order to allow the exploration and development of space to be extended from low-Earth orbit into the solar system. A propellant system using a cryogenic fluid must reduce the amount of unusable propellant due to evaporation and boiling. However, in space exploration and development, where safety and reliability of missions are critical, predictions of the boiling heat transfer of current technology are not sufficiently reliable for thermal management design due to a lack of knowledge and relevant research. Therefore, the objective of this research is to understand and accurately predict boiling heat transfer by developing numerical simulation tools for two-phase flows that consider phase change. In this paper, recent research activity toward the development of chill-down process simulation technology is presented.</p>
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Physics Procedia, 81 158-161, 2016 Peer-reviewed
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TEION KOGAKU (Journal of Cryogenics and Superconductivity Society of Japan), 51(5) 155-163, 2016 Peer-reviewedThe research and development conducted regarding fully superconducting motors for liquid-hydrogen transfer pumps using MgB<sub>2</sub> monofilamentary wires are gathered into this paper. Synchronous rotation without slip can be realized using squirrelcage-type rotor windings composed of quasi-superconducting loops soldered between MgB<sub>2</sub> wires, thereby enabling superconducting motors with low loss and high efficiency to be achieved. The use of MgB<sub>2</sub> wires for stator windings also enables the primary winding loss to be reduced drastically compared to conventional copper winding. The transfer of liquid hydrogen from a metal cryostat containing the fabricated MgB<sub>2</sub> motor to a glass Dewar vessel for visual monitoring is demonstrated successfully.<tt> </tt>
Misc.
170-
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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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 63rd, 2024
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