日本地球惑星科学連合2024年大会

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[J] 口頭発表

セッション記号 P (宇宙惑星科学) » P-EM 太陽地球系科学・宇宙電磁気学・宇宙環境

[P-EM16] 太陽圏・惑星間空間

2024年5月29日(水) 09:00 〜 10:00 展示場特設会場 (2) (幕張メッセ国際展示場 6ホール)

コンビーナ:岩井 一正(名古屋大学 宇宙地球環境研究所)、成行 泰裕(富山大学学術研究部教育学系)、西野 真木(宇宙航空研究開発機構宇宙科学研究所)、坪内 健(電気通信大学)、座長:成行 泰裕(富山大学学術研究部教育学系)、西野 真木(宇宙航空研究開発機構宇宙科学研究所)


09:15 〜 09:30

[PEM16-08] 2022年3月に発生したSEPイベントのBepiColomboおよびSTELEO衛星による観測と数値モデリング

*簑島 敬1三好 由純2村上 豪3岩井 一正2今田 晋亮4 (1.海洋研究開発機構 数理科学・先端技術研究開発センター、2.名古屋大学 宇宙地球環境研究所、3.宇宙航空研究開発機構、4.東京大学 大学院理学系研究科)

キーワード:太陽高エネルギー粒子、多点衛星観測、輸送方程式

Solar Energetic Particles (SEPs) are high-energy charged particles spanning from a few keV to several GeV, which are generated in association with energetic phenomena on the Sun (flares and CMEs), and then are ejected into interplanetary space. Given that SEPs offer insights into acceleration and transport mechanisms in collisionless plasmas, understanding their origin and dynamics is of great interest to space plasma physics and relevant fields (e.g., high-energy astrophysics and laser plasma physics). Furthermore, accurate prediction of the SEP profile is required for space weather operations, as SEPs exceeding 10 MeV pose primary threats to the space environment, including radio communication failure, malfunction and degradation of equipment onboard aircraft and satellites, and radiation exposure of astronauts during extravehicular activities. This is expected to become more and more important in the future as humanity expands its activity beyond the Earth's magnetosphere.
Unraveling the SEP physics presents a formidable challenge. On the theoretical front, the rigorous description of SEPs requires a first-principle kinetic treatment while the system scale of the Sun-Earth environment is far beyond the magnetohydrodynamic scale. On the observational front, SEPs have been conventionally observed by in-situ measurement of an individual satellite, resulting in information about physical mechanisms of acceleration and transport of SEPs being convolved during their journey from the Sun to the observation point. Presently, many satellites are operating to measure SEPs at different radii and longitudes, giving a valuable opportunity to integrate theoretical modeling with multi-satellite observations to extract their physical knowledge.
M and X-class flares, along with subsequent CMEs, occurred on 28 and 30 March, 2022. The propagations of CMEs and background solar wind were reconstructed by the global MHD simulation of the heliosphere based on the ground-based interplanetary scintillation (IPS) observation, IPS-SUSANOO. Two associated SEP events were observed simultaneously by BepiColombo at 0.6 AU and STEREO A at 1 AU. Fortunately, both satellites were positioned approximately along the same Parker spiral. In both events, the Solar Particle Monitor onboard BepiColombo/MMO detected 40-200 MeV ions approximately within one hour after the flare, with their peak exhibiting velocity dispersion indicative of ballistic motion. Time-of-flight analysis suggests the expected starting point to be 0.5-0.7 AU from the BepiColombo, close to the Sun. This is corroborated by the same analysis of 1.8-10 MeV ions detected by the Low Energy Telescope (LET) onboard STEREO A. The BepiColombo Environment Radiation Monitor (BERM) detected 1.5 MeV ions, providing a comparative study with 1.8 MeV ions detected by LET. While the difference in their peak times suggests ballistic motion along the magnetic field, the decay profile observed by LET is more prolonged than that observed by BERM. This observation may imply an increase in scattering over time, potentially indicating a reduction in mean free path to below 0.4 AU, as inferred from focused transport simulations. In this paper, we will present detailed observations and numerical modelling results, and discuss potential scenarios for the transport of SEPs between BepiColombo and STEREO locations.