研究者業績
基本情報
- 所属
- 国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所 太陽系科学研究系 准教授
- 学位
- 博士(理学)
- J-GLOBAL ID
- 200901058783588460
- researchmap会員ID
- 1000292024
研究分野
1経歴
2-
2019年6月 - 現在
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1999年4月
学歴
2-
1995年4月 - 1997年3月
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1991年4月 - 1995年3月
委員歴
3-
2022年4月 - 現在
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2019年4月 - 2025年3月
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2020年4月 - 2022年3月
論文
236-
Earth, Planets and Space 2026年3月13日 査読有りAbstract Electron conics are a distinct type of electron distribution observed in Earth’s magnetosphere, characterized by enhanced fluxes of upgoing electrons at several-keV energies, particularly in the auroral acceleration region. This study analyzes high-altitude (27,000–32,000 km) observations made by the Arase satellite to investigate the characteristics of electron conics after passing through the heating region, employing the high angular resolution of the low-energy particle experiments—electron analyzer (LEPe) onboard the satellite. We analyzed eight electron conic events between 2017 and 2022 to estimate their source altitudes using mirror ratios and potential differences and by comparing pre- and post-heating data to investigate heating properties. Our results show that the source region of conics has an upper boundary at 9,000–14,000 km, with the peak flux originating from a central altitude of 3,000–7,000 km. This region spatially coincides with the source of auroral kilometric radiation (AKR): the central altitude of the source of conics corresponds to the lower boundary of the AKR source, suggesting that a longer residence time of particles within the AKR source region leads to stronger heating. The comparison of pre- and post-heating populations demonstrated that upgoing conic electrons exhibit higher temperatures and lower densities. The number flux remains conserved, indicating the energization of a magnetospheric population, whereas the energy flux is enhanced by up to a factor of four, significantly higher than that reported in previous studies. A test particle simulation, using observed plasma parameters and incorporating stochastic perpendicular heating, reproduces the main features of observed conics in terms of both energy and pitch angle. Our simulation shows that electron conics evolve into narrow, field-aligned beams at higher altitudes, suggesting that some of the anti-Earthward-flowing beams observed in the magnetotail may actually be unresolved conics. These findings contribute to the understanding of energy transport between the auroral acceleration region and the magnetotail and show the importance of high-angular-resolution instrumentation. Graphical Abstract
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Nature Geoscience 2026年2月27日 査読有り
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Journal of Geophysical Research: Space Physics 131(3) 2026年2月24日 査読有り
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Acta Astronautica 2026年1月 査読有り
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Journal of Geophysical Research: Space Physics 130(10) 2025年10月 査読有りAbstract Using Arase satellite observations, this study provides a comprehensive statistical analysis of ions (H+, He+, O+) and electron contributions to the total ring current pressure during storms with two different drivers. The results demonstrate the effect of different solar wind drivers on the composition, energy distribution, and spatial characteristics of the ring current. Using 32 CIR‐ and 30 Interplanetary Coronal Mass Ejection (ICME)‐driven storms, we characterize the ring current pressure evolution during the prestorm, main, early‐recovery, and late‐recovery storm phases as a function of magnetic local time and L‐shell. In CIR‐driven storms, H+ ions are the dominant (∼70%) contributor to the total ring current pressure during main/early recovery phases and increasing to ∼80% during late recovery. In contrast, the O+ pressure (E = 20–50 keV) response is significantly stronger in ICME‐driven storms contributing ∼40% to the overall pressure during the main/early recovery phases and even dominate (∼53%) in certain MLT sectors. Additionally, ICME‐driven storms tend to have peak pressure at lower L‐shells (L ≈ 3–4), while CIR‐driven storms show pressure peaks at slightly higher L‐shells (L ≈ 4–5). Interestingly, electron pressure also plays a notable role in specific MLT sectors, contributing ∼18% (03–09 MLT) during the main phase of CIR‐driven storms and ∼11% (21–03 MLT) during ICME‐driven storms. The results highlight that the storm time electron pressure plays a crucial role in the ring current buildup. Another noteworthy feature of this study is that Arase's fine‐energy resolution and broad coverage enable a detailed investigation of energy‐dependent ring current dynamics.
MISC
144-
極域科学・宙空圏・気水圏・生物・地学シンポジウム講演予稿集(CD−ROM) 2010 ROMBUNNO.PU01 2010年
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極域科学・宙空圏・気水圏・生物・地学シンポジウム講演予稿集(CD−ROM) 2010 ROMBUNNO.PU02 2010年
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地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 128th ROMBUNNO.B006-04 2010年
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 8(ists27(ISTS Special Issue: Sel) Tm_1-Tm6-Tm_6 2010年 査読有り
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地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 124th 2008年
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地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 124th ROMBUNNO.B006-18 2008年
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電子情報通信学会技術研究報告. SANE, 宇宙・航行エレクトロニクス 107(2) 43-48 2007年4月9日This paper describes the on-orbit results and lessons learned of the small scientific satellite "INDEX" (REIMEI) for aurora observation and demonstration of advanced satellite technologies. REIMEI is a small satellite with 72kg mass, and is provided with three-axis attitude controlled capabilities for aurora observation. REIMEI was launched into a nearly sun synchronous polar orbit on Aug. 23^<rd>, 2005 (UT) from Baikonur, Kazakhstan by Dnepr rocket. REIMEI satellite functions satisfactorily on the orbit. Three axis control is achieved with accuracy of 0.05 deg. Multi-spectrum images of aurora are taken with 8Hz rate and 2 km spatial resolution to investigate the aurora physics. REIMEI is a small scientific satellite for aurora observation and advanced satellite technologies, and was launched into a nearly sun synchronous polar orbit on Aug. 23^<rd>, 2005 (UTC) from Baikonur, Kazakhstan by Dnepr rocket. REIMEI satellite functions satisfactorily on the orbit. The three-axis attitude control is achieved with accuracy of 0.05deg. REIMEI is performing the simultaneous observation of aurora images as well as particle measurements. REIMEI indicates that even a small satellite launched as a piggy-back can successfully perform the unique scientific mission purposes.
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ICARUS 187(2) 623-625 2007年4月
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地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 122nd ROMBUNNO.B006-40 2007年
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SPACE SCIENCE REVIEWS 126(1-4) 333-354 2006年10月
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SPACE SCIENCE REVIEWS 126(1-4) 239-266 2006年10月
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SPACE SCIENCE REVIEWS 126(1-4) 113-164 2006年10月
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電子情報通信学会技術研究報告. SANE, 宇宙・航行エレクトロニクス 105(438) 29-34 2005年11月25日小型科学衛星INDEX(れいめい)の打上げと初期成果
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European Space Agency, (Special Publication) ESA SP (1240) 121-139 2004年8月
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地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 110th (Web) 2001年
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REVIEW OF SCIENTIFIC INSTRUMENTS 71(8) 3024-3030 2000年8月
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GEOPHYSICAL RESEARCH LETTERS 26(1) 33-36 1999年1月
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ISAS Research Note 607 1997年
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JOURNAL OF GEOMAGNETISM AND GEOELECTRICITY 47(10) 973-987 1995年
共同研究・競争的資金等の研究課題
20-
日本学術振興会 科学研究費助成事業 2025年4月 - 2030年3月
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日本学術振興会 科学研究費助成事業 2022年10月 - 2027年3月
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日本学術振興会 科学研究費助成事業 基盤研究(A) 2021年4月 - 2026年3月
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日本学術振興会 科学研究費助成事業 挑戦的研究(萌芽) 2022年6月 - 2025年3月
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日本学術振興会 科学研究費助成事業 基盤研究(B) 2021年4月 - 2024年3月