Japan Geoscience Union Meeting 2025

Presentation information

[E] Oral

P (Space and Planetary Sciences ) » P-CG Complex & General

[P-CG20] Future missions and instrumentation for space and planetary science

Thu. May 29, 2025 1:45 PM - 3:15 PM 303 (International Conference Hall, Makuhari Messe)

convener:Takefumi Mitani(Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science), Masaki Kuwabara(Rikkyo University), Shoichiro Yokota(Graduate School of Science, Osaka University), Yuichiro Cho(Department of Earth and Planetary Science, University of Tokyo), Chairperson:Shoichiro Yokota(Graduate School of Science, Osaka University), Takefumi Mitani(Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science)


1:45 PM - 2:00 PM

[PCG20-13] IMPACT Project: A Microsatellite Mission to Investigate Ducting Magnetospheric Plasma Wave Activity

★Invited Papers

*Shoya Matsuda1, Satoshi Yagitani1, Daisuke Yonetoku1, Yoshiya Kasahara1, Tomohiko Imachi1, Yasuhiro Shoji1, Tatsuya Sawano1, Makoto Arimoto1, Mitsunori Ozaki1, Mariko Kimura1, Yuto Katoh2, Atsushi Kumamoto2, Satoshi Kasahara3, Hirotsugu Kojima4, Satoshi Kurita4, Yoshiharu Omura4, Yoshizumi Miyoshi5, Mariko Teramoto6, Kentarou Kitamura6, Shinji Saito7, Iku Shinohara8, Kazushi Asamura8, Takefumi Mitani8 (1.Kanazawa University, 2.Tohoku University, 3.The University of Tokyo, 4.Kyoto University, 5.Nagoya University, 6.Kyushu Institute of Technology, 7.NICT, 8.ISAS/JAXA)

Keywords:Microsatellite mission, Plasma waves, Space weather

The IMPACT project is a microsatellite project aimed at clarifying the formation mechanisms of density ducts in the terrestrial inner magnetosphere and wave-particle interactions induced by plasma waves propagating through these ducts. This project was selected for the JAXA-SMASH (JAXA-Small Satellite Rush) Program in February 2025, and the development of the microsatellite is ongoing by early 2027. This satellite is a W6U-size CubeSat and carries three scientific instruments: a small plasma wave detector (DPS), a small high-energy electron detector (LEON), and a small impedance probe (NEI). This instrument suite provides direct measurements of the density duct structure, plasma waves propagating through the ducts, and radiation belt electrons scattered by electromagnetic ion cyclotron waves traveling through the ducts. The satellite system is controlled by AI-OBC, which is an onboard computer equipped with a dynamically reconfigurable processor. AI-OBC enables high-speed inference using deep learning models in space to detect duct structures and plasma waves. In this study, we will introduce the overview of the IMPACT project and the latest updates.