研究者業績

藤本 龍一

フジモト リュウイチ  (Ryuichi Fujimoto)

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 宇宙物理学研究系 教授
総合研究大学院大学 先端学術院 宇宙科学コース 教授
東京工業大学 理学院 特定教授
学位
博士(理学)(東京大学)
修士(東京大学)

研究者番号
20280555
ORCID ID
 https://orcid.org/0000-0002-2374-7073
J-GLOBAL ID
200901095989600566
researchmap会員ID
1000363020

X線マイクロカロリメータを用いた極低温精密X線分光装置の開発に取り組み,2023年9月打ち上げのXRISM衛星に搭載されたResolve観測装置として実現しました.

研究指導のテーマとしては,(1) XRISM衛星による精密X線分光観測データを解析し,銀河団ガスの運動を調べて,宇宙の大規模構造形成過程の理解を深める,(2) 宇宙マイクロ波背景放射の偏光観測を目指すLiteBIRD衛星を見据えた実験的研究を行なう等.特定の自然現象について理解を深めると同時に,複雑な自然現象の背景にある物理法則に至る過程を,実験・解析手法とともにしっかりと身につけてもらいたいと考えています.


学歴

 4

委員歴

 2

論文

 155
  • Seiji Yoshida, Masahito Isshiki, Ken'ichi Kanao, Shoji Tsunematsu, Kiyomi Otsuka, Syou Mizunuma, Yoh Takei, Akio Hoshino, Ryuichi Fujimoto, Yuichiro Ezoe, Kosuke Sato, Michael DiPirro, Peter Shirron
    Cryogenics 139 103831-103831 2024年4月  査読有り
  • Hasebe, T., Imamura, R., Tsujimoto, M., Awaki, H., Chiao, M.P., Fujimoto, R., Hartz, L.S., Kilbourne, C.A., Sneiderman, G.A., Takei, Y., Yasuda, S.
    Journal of Astronomical Telescopes, Instruments, and Systems 9(1) 14003-14003 2023年  
  • K. Sato, N. Y. Yamasaki, M. Ishida, Y. Maeda, K. Mitsuda, Y. Ishisaki, Y. Fujita, Y. Ezoe, I. Mitsuishi, Y. Tawara, K. Osato, N. Kawai, K. Matsushita, D. Nagai, K. Yoshikawa, R. Fujimoto, T. G. Tsuru, N. Ota, S. Yamada, Y. Ichinohe, Y. Uchida, Y. Nakashima
    Journal of Low Temperature Physics 209(5-6) 971-979 2022年12月  
  • Kosuke Sato, Noriko Y. Yamasaki, Shinya Yamada, Ikuyuki Mitsuishi, Yuto Ichinohe, Hajime Omamiuda, Yuusuke Uchida, Kazuhisa Mitsuda, Daisuke Nagai, Kohji Yoshikawa, Ken Osato, Kyoko Matsushita, Yutaka Fujita, Yoshitaka Ishisaki, Yuichiro Ezoe, Manabu Ishida, Yoshitomo Maeda, Nobuyuki Kawai, Ryuichi Fujimoto, Takeshi G. Tsuru, Naomi Ota, Yuki Nakashima
    Space Telescopes and Instrumentation 2022: Ultraviolet to Gamma Ray 12181 2022年8月31日  
  • Takashi Hasebe, Ryuta Imamura, Masahiro Tsujimoto, Hisamitsu Awaki, Meng P. Chiao, Ryuichi Fujimoto, Leslie S. Hartz, Gary A. Sneiderman, Yoh Takei, Susumu Yasuda
    Proceedings of SPIE - The International Society for Optical Engineering 12181 2022年  
    Resolve is a payload hosting an x-ray microcalorimeter detector operated at 50 mK in the X-Ray Imaging and Spectroscopy Mission (XRISM), which is currently under development by an international collaboration and is planned to be launched in 2023. One of the technical concerns is the micro-vibration interference to the sensitive microcalorimeter detector by the spacecraft bus components. We verified this in a series of the ground tests in 2021–2022, the results of which are reported here. We defined the micro-vibration interface between the spacecraft and the Resolve instrument. In the instrument-level test, we tested the flight-model hardware against the interface level by injecting micro-vibration using vibrators and evaluated the instrument response using the 50 mK stage temperature stability, the ADR magnet current consumption rate, and the detector noise spectra. We found the strong responses when injecting micro-vibration at ∼200, 380, and 610 Hz. In the former two cases, the beat among the injected frequency and the cryocooler frequency harmonics are also observed in the detector noise spectra. In the spacecraft-level test, we measured the acceleration and the instrument responses with and without suspending the entire spacecraft. The reaction wheels and the inertial reference units, two major sources of micro-vibration among the bus components, were operated. We found that the observed Resolve responses are within acceptable levels.

MISC

 129

共同研究・競争的資金等の研究課題

 20