Curriculum Vitaes
Profile Information
- Affiliation
- Associate Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- Ph(Mar, 2013, The University of Tokyo)
- Researcher number
- 70720697
- ORCID ID
https://orcid.org/0000-0002-6265-1672- J-GLOBAL ID
- 202001010789612597
- researchmap Member ID
- R000013995
Research Interests
6Research Areas
1Research History
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Sep, 2016 - Oct, 2017
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Apr, 2013 - Jul, 2013
Education
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Apr, 2000 - Mar, 2003
Committee Memberships
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Apr, 2023 - Present
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Apr, 2022 - Mar, 2024
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Apr, 2019 - Mar, 2020
Awards
15-
May, 2024
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Apr, 2021
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Dec, 2020
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Sep, 2020
Papers
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Journal of Applied Physics, 135(24), Jun 27, 2024 Peer-reviewedIonic liquid electrospray thrusters represent an alternative propulsion method for spacecraft to conventional plasma propulsion because they do not require plasma generation, which significantly increases the thrust efficiency. The porous emitter thruster has the advantages of simple propellant feeding and multi-site emissions, which miniaturize the thruster size and increase thrust. However, the multi-scale nature, that is, nano- to micrometer-sized menisci on the millimeter-size porous needle tip, makes modeling multi-site emissions difficult, and direct observation is also challenging. This paper proposes a simple model for multi-site emissions, which assumes that the ionic conductivity or ion transport in the porous media determines the ion-emission current. The conductivity was evaluated by comparing the experimental and numerical data based on the model. The results suggest that the ionic conductivity of the porous emitter is suppressed by the ion–pore wall friction stress. Additionally, the model indicates that the emission area expansion on the porous emitter creates the unique curve shape of the current vs voltage characteristics for multi-site emissions.
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AIP Advances, 14(6), Jun 1, 2024 Peer-reviewedAn understanding of the degradation mechanism of a microwave discharge cathode is the key to extending the lifetime of microwave ion thruster systems. This study investigates the effect of nozzle contamination by sputtered Ag-polytetrafluoroethylene (PTFE) on microwave discharge cathode performance. The current–voltage characteristics were measured for nominal and contaminated (by PTFE spray with 0.2 µm thick or tape with 0.15 mm thick) cathodes. The contamination thickness and area on the nozzle were varied to investigate the characteristic differences. It was confirmed that the anode voltage increased by 20 V or more in the case of the contaminated cathode. The anode voltage was measured for the sputter-contaminated cathode to evaluate the effect of contamination under more realistic conditions. After 630 h of sputter-contamination operation, it is estimated that sputtered particles were deposited to a thickness of 77 µm at most, and the anode voltage increased by 8 V. The results show that the downstream surface of the nozzle is critical for maintaining cathode performance. The insulating coating formed by the sputtered PTFE may interfere with ion absorption and degrade electron emission capability. A theoretical model based on the extended Brophy model supports these results. This study provides important information for the use of PTFE-based materials around ion thrusters.
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Acta Astronautica, May, 2024 Peer-reviewed
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Vacuum, 220 112760-112760, Feb, 2024 Peer-reviewed
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Acta Astronautica, 212 130-138, Nov, 2023 Peer-reviewed
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Acta Astronautica, Jul, 2023 Peer-reviewed
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Journal of Evolving Space Activities, 1 21, Jun, 2023 Peer-reviewed
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Journal of Evolving Space Activities, 1, Apr, 2023 Peer-reviewed
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Science (New York, N.Y.), 379(6634) eabn7850, Feb 24, 2023 Peer-reviewedCarbonaceous meteorites are thought to be fragments of C-type (carbonaceous) asteroids. Samples of the C-type asteroid (162173) Ryugu were retrieved by the Hayabusa2 spacecraft. We measured the mineralogy and bulk chemical and isotopic compositions of Ryugu samples. The samples are mainly composed of materials similar to those of carbonaceous chondrite meteorites, particularly the CI (Ivuna-type) group. The samples consist predominantly of minerals formed in aqueous fluid on a parent planetesimal. The primary minerals were altered by fluids at a temperature of 37° ± 10°C, about [Formula: see text] million (statistical) or [Formula: see text] million (systematic) years after the formation of the first solids in the Solar System. After aqueous alteration, the Ryugu samples were likely never heated above ~100°C. The samples have a chemical composition that more closely resembles that of the Sun's photosphere than other natural samples do.
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Science (New York, N.Y.), 379(6634) eabo0431, Feb 24, 2023 Peer-reviewedThe near-Earth carbonaceous asteroid (162173) Ryugu is expected to contain volatile chemical species that could provide information on the origin of Earth's volatiles. Samples of Ryugu were retrieved by the Hayabusa2 spacecraft. We measured noble gas and nitrogen isotopes in Ryugu samples and found that they are dominated by presolar and primordial components, incorporated during Solar System formation. Noble gas concentrations are higher than those in Ivuna-type carbonaceous (CI) chondrite meteorites. Several host phases of isotopically distinct nitrogen have different abundances among the samples. Our measurements support a close relationship between Ryugu and CI chondrites. Noble gases produced by galactic cosmic rays, indicating a ~5 million year exposure, and from implanted solar wind record the recent irradiation history of Ryugu after it migrated to its current orbit.
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Science (New York, N.Y.), 379(6634) eabn9057, Feb 24, 2023 Peer-reviewedSamples of the carbonaceous asteroid (162173) Ryugu were collected and brought to Earth by the Hayabusa2 spacecraft. We investigated the macromolecular organic matter in Ryugu samples and found that it contains aromatic and aliphatic carbon, ketone, and carboxyl functional groups. The spectroscopic features of the organic matter are consistent with those in chemically primitive carbonaceous chondrite meteorites that experienced parent-body aqueous alteration (reactions with liquid water). The morphology of the organic carbon includes nanoglobules and diffuse carbon associated with phyllosilicate and carbonate minerals. Deuterium and/or nitrogen-15 enrichments indicate that the organic matter formed in a cold molecular cloud or the presolar nebula. The diversity of the organic matter indicates variable levels of aqueous alteration on Ryugu's parent body.
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Science (New York, N.Y.), 379(6634) eabn9033, Feb 24, 2023 Peer-reviewedThe Hayabusa2 spacecraft collected samples from the surface of the carbonaceous near-Earth asteroid (162173) Ryugu and brought them to Earth. The samples were expected to contain organic molecules, which record processes that occurred in the early Solar System. We analyzed organic molecules extracted from the Ryugu surface samples. We identified a variety of molecules containing the atoms CHNOS, formed by methylation, hydration, hydroxylation, and sulfurization reactions. Amino acids, aliphatic amines, carboxylic acids, polycyclic aromatic hydrocarbons, and nitrogen-heterocyclic compounds were detected, which had properties consistent with an abiotic origin. These compounds likely arose from an aqueous reaction on Ryugu's parent body and are similar to the organics in Ivuna-type meteorites. These molecules can survive on the surfaces of asteroids and be transported throughout the Solar System.
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Nature astronomy, 7(2) 170-181, 2023 Peer-reviewed
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Journal of Electric Propulsion, 1(1), Dec, 2022 Peer-reviewedInvitedAbstract In electron cyclotron resonance (ECR) thrusters, the plasma mode transition is a critical phenomenon because it determines the maximum thrust performance. In ECR ion thrusters, ionization generally occurs in the magnetic confinement region, where electrons are continuously heated by ECR and confined by magnetic mirrors. However, as the flow rate increases, ionization is also observed outside the magnetic confinement region, and this induces the plasma mode transition. In our previous work, two-photon absorption laser-induced fluorescence (TALIF) analysis revealed that the stepwise ionization from the metastable state plays an important role in the ionization process. However, the distribution of the stepwise ionization has not yet been revealed because of the long lifetime of the metastable state. In this study, this distribution was investigated using one experimental and two numerical approaches. First, TALIF was applied to two types of gas injection with clear differences in thrust performance and ground-state neutral density distribution. In the first simulation, the metastable state particle simulation was used to estimate the excitation rate distribution. In the second study, simulations of the electric field of microwaves were used to estimate the contribution of the stepwise ionization to the plasma density. The experimental and numerical results revealed that the stepwise ionization spreads outside the magnetic confinement region because of the diffusion of metastable particles, and this spread induces the plasma mode transition, explaining the difference between the two types of gas injection.
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Science advances, 8(46) eabo7239, Nov 18, 2022 Peer-reviewed
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NATURE ASTRONOMY, 6(10) 1163-+, Oct, 2022 Peer-reviewed
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Vacuum, 200 110962-110962, Jun, 2022 Peer-reviewed
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Hayabusa2 Asteroid Sample Return Mission, 401-414, Apr, 2022 Peer-reviewed
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Science, 375(6584) 1011-1016, Mar 4, 2022 Peer-reviewed
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Nature Astronomy, 6(2) 214-220, Feb, 2022 Peer-reviewed
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Journal of Applied Physics, 131(1) 013301-013301, Jan 7, 2022 Peer-reviewedInvited
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Review of Scientific Instruments, 92(12) 129902-129902, Dec 1, 2021 Peer-reviewed
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The Review of scientific instruments, 92(11) 114501-114501, Nov 1, 2021 Peer-reviewed
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Investigation of plasma mode transition and hysteresis in electron cyclotron resonance ion thrustersPlasma Sources Science and Technology, 30(9) 095023-095023, Sep 1, 2021 Peer-reviewed
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Acta Astronautica, 185 179-187, Aug, 2021 Peer-reviewed
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VACUUM, 190, Aug, 2021 Peer-reviewed
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Acta Astronautica, 181 14-27, Apr, 2021 Peer-reviewed
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JOURNAL OF PROPULSION AND POWER, 37(2) 223-230, Mar, 2021 Peer-reviewed
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 64(3) 189-192, 2021 Peer-reviewed
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Nature Astronomy, 5(3) 246-250, 2021 Peer-reviewed
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Nature Astronomy, 5(1) 39-45, Jan, 2021 Peer-reviewed
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Astrodynamics, 4(4) 349-375, Dec, 2020 Peer-reviewed
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ACTA ASTRONAUTICA, 176 413-423, Nov, 2020 Peer-reviewed
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ACTA ASTRONAUTICA, 176 77-88, Nov, 2020 Peer-reviewed
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ACTA ASTRONAUTICA, 174 367-376, Sep, 2020 Peer-reviewed
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JOURNAL OF PROPULSION AND POWER, 36(4) 586-592, Jul, 2020 Peer-reviewed
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Science, 368(6491) 654-659, May 8, 2020 Peer-reviewed
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Science, 368(6486), Apr, 2020 Peer-reviewed
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NATURE, 579(7800) 518-522, Mar, 2020 Peer-reviewed
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 18(3) 57-63, 2020 Peer-reviewed<p>The authors investigate the discharge chamber of the microwave ion thruster μ10 by using kinetic particle simulation. First, to investigate the plasma phenomena qualitatively, we conduct a particle-in-cell (PIC) simulation model. The simulation results indicate that the distribution of ion density is ring-shaped. To verify the simulation result with the experimental result, the simulation result is compared with the optical emission distribution. In low propellant flow rates, the distribution of ion density agrees with the optical emission distribution. However, in high propellant flow rates, the optical emission distribution is different from simulation results in the waveguide due to the excited neutral particles. In the thruster, the performance strongly depends on the location of injecting the propellant. Hence, to develop the plasma simulation for quantitative comparison with the experiment, the distribution of the neutral density is evaluated by using direct Monte Carlo simulation (DSMC). The results show the neutral density in the waveguide increases corresponding to the ratio of waveguide injection, which indicates that the density is one of the most important parameters for quantitative evaluation with the experiment.</p>
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ACTA ASTRONAUTICA, 166 69-77, Jan, 2020 Peer-reviewed
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 63(6) 281-283, 2020 Peer-reviewed
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Space Solar Power Systems, 5 101-106, 2020 Peer-reviewed<p> Mass and cost of In-space transportation systems are investigated parametrically. Analytical investigation shows the cost-optimum thruster specific impulse is smaller than that of the cost-optimum one. Sensitivity analysis reveals that the specific mass, kg/kW of the power system and propulsion system, has dominant influence on the mass and cost of the orbital transfer system. It is also argued that the GTO to GEO scenario is more mass and cost effective than that of the LEO to GEO one, unless the specific mass is drastically improved than the state-of-the-art.</p>
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ACTA ASTRONAUTICA, 165 25-31, Dec, 2019 Peer-reviewed
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REVIEW OF SCIENTIFIC INSTRUMENTS, 90(10), Oct, 2019 Peer-reviewed
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VACUUM, 168, Oct, 2019 Peer-reviewed
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ACTA ASTRONAUTICA, 161 382-388, Aug, 2019 Peer-reviewed
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Physics of Plasmas, 26(7), Jul 1, 2019 Peer-reviewed
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JOURNAL OF PROPULSION AND POWER, 35(3) 565-571, May, 2019 Peer-reviewed
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Acta Astronautica, 157 425-434, Apr, 2019 Peer-reviewed
Misc.
110-
宇宙科学技術連合講演会講演集(CD-ROM), 67th, 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 In the 3D-printed resistojet that the authors are working on, it is necessary to provide an electrical contact point at a high temperature part considering the limitations in 3D printing. So far, we have made some prototypes of flat contact type, tapered contact type, and screw type. In addition, as a new attempt, we also describe design guidelines for banana plug type that contact with radial surface pressure. 資料番号: SA6000184068 STEP-2022-016
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日本航空宇宙学会誌 = Aeronautical and space sciences Japan, 70(10) 214-217, Oct, 2022
Books and Other Publications
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Elsevier, 2022 (ISBN: 9780323997317)
Teaching Experience
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Dec, 2022 - Jan, 2023Advanced Energy Conversion (Graduate School of Frontier Sciences, The University of Tokyo)
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Sep, 2021 - Feb, 2022Propulsion and Energy Systems (Graduate School of Frontier Sciences The University of Tokyo)
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Sep, 2021 - Nov, 2021Propulsion and Energy Systems (The University of Tokyo)
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Sep, 2013 - Mar, 2016Earth and Astronomical Science (Komazawa Women's University)
Professional Memberships
3-
Jul, 2011 - Present
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Sep, 2009 - Present
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Apr, 2008 - Present
Research Projects
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, 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, 2023 - Mar, 2027
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2023 - Mar, 2027
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Grants-in-Aid for Scientific Research Grant-in-Aid for Young Scientists (A), Japan Society for the Promotion of Science, Apr, 2017 - Mar, 2021
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Grants-in-Aid for Scientific Research Grant-in-Aid for Young Scientists (B), Japan Society for the Promotion of Science, Apr, 2014 - Mar, 2017
Industrial Property Rights
2Academic Activities
1Media Coverage
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J-WAVE, JK Radio Tokyo United, https://www.j-wave.co.jp/original/tokyounited/archives/the-hidden-story/2021/02/19-111253.html, Feb, 2021 TV or radio program