Curriculum Vitaes
Profile Information
- Affiliation
- Professer, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- Ph. D(Mar, 1998, Waseda University)
- J-GLOBAL ID
- 200901062235719944
- researchmap Member ID
- 1000320874
Research Interests
4Research Areas
4Education
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- 1998
Papers
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Journal of Geophysical Research: Space Physics, 129(12), Dec 13, 2024Abstract We investigate the dynamics of relativistic electrons in the Earth's outer radiation belt by analyzing the interplay of several key physical processes: electron losses due to pitch angle scattering from electromagnetic ion cyclotron (EMIC) waves and chorus waves, and electron flux increases from chorus wave‐driven acceleration of 100–300 keV seed electrons injected from the plasma sheet. We examine a weak geomagnetic storm on 17 April 2021, using observations from various spacecraft, including GOES, Van Allen Probes, ERG/ARASE, MMS, ELFIN, and POES. Despite strong EMIC‐ and chorus wave‐driven electron precipitation in the outer radiation belt, trapped 0.1–1.5 MeV electron fluxes actually increased. We use theoretical estimates of electron quasi‐linear diffusion rates by chorus and EMIC waves, based on statistics of their wave power distribution, to examine the role of those waves in the observed relativistic electron flux variations. We find that a significant supply of 100–300 keV electrons by plasma sheet injections together with chorus wave‐driven acceleration can overcome the rate of chorus and EMIC wave‐driven electron losses through pitch angle scattering toward the loss cone, explaining the observed net increase in electron fluxes. Our study emphasizes the importance of simultaneously taking into account resonant wave‐particle interactions and modeled local energy gradients of electron phase space density following injections, to accurately forecast the dynamical evolution of trapped electron fluxes.
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Journal of Geophysical Research: Space Physics, 129(11), Oct 28, 2024Abstract Near‐equatorial measurements of energetic electron fluxes, in combination with numerical simulation, are widely used for monitoring of the radiation belt dynamics. However, the long orbital periods of near‐equatorial spacecraft constrain the cadence of observations to once per several hours or greater, that is, much longer than the mesoscale injections and rapid local acceleration and losses of energetic electrons of interest. An alternative approach for radiation belt monitoring is to use measurements of low‐altitude spacecraft, which cover, once per hour or faster, the latitudinal range of the entire radiation belt within a few minutes. Such an approach requires, however, a procedure for mapping the flux from low equatorial pitch angles (near the loss cone) as measured at low altitude, to high equatorial pitch angles (far from the loss cone), as necessitated by equatorial flux models. Here we do this using the high energy resolution ELFIN measurements of energetic electrons. Combining those with GPS measurements we develop a model for the electron anisotropy coefficient, , that describes electron flux dependence on equatorial pitch‐angle, , . We then validate this model by comparing its equatorial predictions from ELFIN with in‐situ near‐equatorial measurements from Arase (ERG) in the outer radiation belt.
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Journal of Evolving Space Activities, 2 n/a, 2024The Institute of Space and Astronautical Science (ISAS) of the Japan Aerospace Exploration Agency (JAXA) conducts a deep space exploration mission named Demonstration and Experiment of Space Technology for INterplanetary voYage with Phaethon fLyby and dUst Science (DESTINY+). The mission requires a high-performance, compact solid kick stage with a high mass ratio and high system safety. The kick stage employes a newly developed laser ignition system to meet these requirements. We designed a laser unit for upper stages (LUUS), two types of laser-initiated pyrotechnic devices for solid motor ignition and a separation device actuator (the LID and LCTG) for the kick stage system. Optical fiber paths connecting the LUUS to LID/LCTG enables a continuity check by optical frequency domain reflectometry (OFDR). We successfully conducted continuity checks with OFDR and ran laser ignition tests to validate the design in simulating assembly- and launchsite operations.
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Earth, Planets and Space, 75(1), Dec 21, 2023Abstract Variations of relativistic electron fluxes (E ≥ 1 MeV) and wave activity in the Earth magnetosphere are studied to determine the contribution of different acceleration mechanisms of the outer radiation belt electrons: ULF mechanism, VLF mechanism, and adiabatic acceleration. The electron fluxes were measured by Arase satellite and geostationary GOES satellites. The ULF power index is used to characterize the magnetospheric wave activity in the Pc5 range. To characterize the VLF wave activity in the magnetosphere, we use data from PWE instrument of Arase satellite. We consider some of the most powerful magnetic storms during the Arase era: May 27–29, 2017; September 7–10, 2017; and August 25–28, 2018. Also, non-storm intervals with a high solar wind speed before and after these storms for comparison are analyzed. Magnitudes of relativistic electron fluxes during these magnetic storms are found to be greater than that during non-storm intervals with high solar wind streams. During magnetic storms, the flux intensity maximum shifts to lower L-shells compared to intervals without magnetic storms. For the considered events, the substorm activity, as characterized by AE index, is found to be a necessary condition for the increase of relativistic electron fluxes, whereas a high solar wind speed alone is not sufficient for the relativistic electron growth. The enhancement of relativistic electron fluxes by 1.5–2 orders of magnitude is observed 1–3 days after the growth of the ULF index and VLF emission power. The growth of VLF and ULF wave powers coincides with the growth of substorm activity and occurs approximately at the same time. Both mechanisms operate at the first phase of electron acceleration. At the second phase of electron acceleration, the mechanism associated with the injection of electrons into the region of the magnetic field weakened by the ring current and their subsequent betatron acceleration during the magnetic field restoration can work effectively. Graphical Abstract
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Journal of Evolving Space Activities, 1, Dec, 2023 Peer-reviewed
Misc.
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宇宙科学技術連合講演会講演集(CD-ROM), 62nd, 2018
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Thermophysical Properties, 39th, 2018
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日本航空宇宙学会中部・関西支部合同秋期大会講演論文集(CD-ROM), 55th, 2018
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宇宙科学技術連合講演会講演集(CD-ROM), 62nd, 2018
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宇宙科学技術連合講演会講演集(CD-ROM), 62nd, 2018
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宇宙科学技術連合講演会講演集(CD-ROM), 62nd ROMBUNNO.3C19, 2018
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日本地球惑星科学連合大会予稿集(Web), 2017, 2017
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応用物理学会春季学術講演会講演予稿集(CD-ROM), 63rd ROMBUNNO.20P‐KD‐7, Mar 3, 2016
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RADIOISOTOPES, 65(2) 81-92, 2016After the nuclear accident in Fukushima Daiichi Power Plant, the technology to visualize radioactive substances has been highly desired to effectively support the radioactive clean-up. In addition to the Si/CdTe semiconductor Compton camera that was proposed and has been developed by our group, we pick up some topics regarding practical visualization systems realized in recent years.
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115(67) 35-38, May 29, 2015
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日本物理学会講演概要集(CD-ROM), 70(1) ROMBUNNO.21PDD-13-417, Mar 24, 2015
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JAXA research and development report, 14 151-160, Mar, 2015Alpha-ray detector (ARD) onboard SELENE was designed for detecting α-particles emitted by Rn-222 emanated on the lunar surface and its descendent nuclear species Po-210. Distribution and variation of radon gas measured by the α-particle signal is expected to provide information on the subsurface uranium distribution, crustal structures including faults, and behavior of the thin atmosphere of the moon. In this paper, we describe the flow of ARD data processing and a method to derive the α-particle intensity distribution utilizing the angular response of the detector which is applied to the radon α-particle observations for the first time. The method improves the resolution of the α-particle intensity map and enables detailed comparison with the geographical features of the lunar surface.
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電子情報通信学会技術研究報告, 115(67(SANE2015 6-15)), 2015
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日本物理学会講演概要集, 69(2) 49-49, Aug 22, 2014
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JPS Conf. Proc., 1(015100), Mar, 2014 Peer-reviewed
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Development of the high‐speed digital processing system by ASIC for HEP‐e on board the ERG satellite電子情報通信学会技術研究報告, 113(367(SANE2013 107-112)) 7-12, Dec 13, 2013The ERG (Energization and Radiation in Geospace) satellite observes Geospace containing the radiation belt which direct observation was not yet fully conducted, and the elucidation of acceleration mechanism of a relativistic particle in Geospace associated with space storm. The particle observation by ERG satellite employs 6 PPE (Plasma particle Experiment) in total, and HEP-e which is one of the PPE instruments the electron of the range from 0.07 to 2 MeV by SSSD. Finally, we establish calculation process using ASIC called VATA for radiation analysis. This VATA for HEP-e on board the ERG has ADC, which is not used in ASIC for HEP on board MMO, realizing more miniaturization and power-saving. However, we still have not yet fully understood about the processing maximum speed in active. It became clear that ASIG can demonstrate the speed of 5.5 kHz at the latest through this quality assessment. Furthermore, even if low on the whole, it was shown for the first time that it can calculate high energetic electrons with the speed of 1.86 kHz.
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電子情報通信学会技術研究報告, 112(330(SANE2012 110-119)) 41-45, Nov 23, 2012ERG (Energization and Radiation in Geospace) satellite will be launched to study acceleration processes of energetic particles in the radiation belt surrounding the earth. It is very important to reveal the acceleration process of high-energy particles for both science and application to space weather forecast. Drastic increase of high-energy electrons in the radiation belt is sometimes observed during a geomagnetic storm. When a large magnetic storm occurs, energetic electron count rate may exceed flux limit expected in the nominal design and large number of incident electrons leads to detection loss. Purpose of this study is to demonstrate that the count rate range of a single detector on board ERG satellite can be expanded by means of reading circuit operation to decrease an area of detection.
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NIRS-M (National Inst. of Radiological Sciences), (251) 243-244, Aug, 2012
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Meeting abstracts of the Physical Society of Japan, 67(1) 126-126, Mar 5, 2012
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NIRS-M (National Inst. of Radiological Sciences), (244) 258-259, Nov, 2011
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Technical report of IEICE. SANE, 111(239) 57-61, Oct 10, 2011Introduction to Geospace Exploration Mission ERG
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111(239) 57-61, Oct, 2011Introduction to Geospace Exploration Mission ERG
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Meeting abstracts of the Physical Society of Japan, 66(1) 124-124, Mar 3, 2011
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Meeting abstracts of the Physical Society of Japan, 65(2) 91-91, Aug 18, 2010
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NIRS-M (National Inst. of Radiological Sciences), (234) 272-273, Jun, 2010
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Proceedings of the IEICE General Conference, 2010(1) SS_85-SS-86, Mar, 2010
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Meeting abstracts of the Physical Society of Japan, 65(1) 108-108, Mar 1, 2010
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Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, 2009 59-59, Sep 28, 2009
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Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, 2009, Sep 28, 2009
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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, 109(101) 59-64, Jun 18, 2009SWIMμνとは,SDS-1衛星のミッション機器の一つであるSWIMに搭載した超小型重力波検出器である.今まで衛星搭載検出器の経験のない,大学の研究室レベルで製作したことが特徴である.SWIMμνは以下の3つの目的を持っている.1.衛星検出器単体としては世界初の重力波探査を行う.2.将来の重力波検出衛星開発に向けた前哨ミッションとなる.3.(検出器は加速度計としてもはたらくため)衛星の振動環境を測定する.SWIMが搭載されたSDS-1衛星は2009年1月23日に無事に地球周回軌道に投入された.その後,SWIMμν内試験質量の観測モードへの制御が成功するなど,順調に運用を行っている.本稿では,そのSWIMμvの開発の背景・その目的と装置の仕組み,また初期運用状況について解説する.
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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, 109(101) 53-58, Jun 18, 2009次世代の通信規格スペースワイヤーを用いた、新しい衛星システム設計の実証モジュールとしてSWIMの開発を行った。さらに、SWIMには、宇宙での実証実験により参加しやすくするための仕組みを構築するという目的がある。今回は、ユーザーモジュールとして超小型の重力波センサーを搭載し、宇宙での実証に望んだ。「いぶき」の相乗り小型衛星として打ち上げられたSDS-1に搭載されたSWIMは2009年2月9日に軌道上でのスペースワイヤー通信の実証に成功するとともに、ユーザーモジュール実験を無事に実施することに成功した。
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IEEE TRANSACTIONS ON NUCLEAR SCIENCE, 56(3) 747-751, Jun, 2009
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Meeting abstracts of the Physical Society of Japan, 64(1) 93-93, Mar 3, 2009
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Meeting Abstracts of the Physical Society of Japan, 64.1.1 100, 2009
Professional Memberships
5Research Projects
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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, 2016 - Mar, 2020
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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, 2014 - Mar, 2017
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Jun, 2012 - Mar, 2017
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Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (A), Japan Society for the Promotion of Science, Apr, 2012 - Mar, 2016