Curriculum Vitaes

Ryuichi Fujimoto

  (藤本 龍一)

Profile Information

Affiliation
Professor, Department of Space Astronomy and Astrophysics, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
Professor, Graduate Institute for Advanced Studies, The Graduate University for Advanced Studies (SOKENDAI)
Visiting Professor, School of Science, Tokyo Institute of Technology
Degree
Ph. D.(The University of Tokyo)
master's degree(The University of Tokyo)

Researcher number
20280555
ORCID ID
 https://orcid.org/0000-0002-2374-7073
J-GLOBAL ID
200901095989600566
researchmap Member ID
1000363020

I have been developing cryogenic high-resolution X-ray microcalorimeter spectrometers onboard X-ray astronomy satellite. It was achieved as the Resolve instrument onboard XRISM, which was launched in September, 2023.

Here are research themes I can provide. (1) Analyze high-resolution X-ray spectroscopy data obtained by XRISM satellite, and research motion of the hot gas in clusters of galaxies, in order to understand the formation of the large-scale structures of the Universe. (2) Conduct experimental studies, in anticipation of LiteBIRD mission, that aims for observing the polarization of the cosmic microwave background radiation.

Message to students: Through the research, develop an understanding of specific natural phenomena, and also learn the process to reach fundamental physics laws that underlie the complex phenomena, together with experimental and/or analytical methods.


Committee Memberships

 2

Papers

 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, Apr, 2024  Peer-reviewed
  • 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  
  • 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, Dec, 2022  
  • 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, Aug 31, 2022  
  • 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  
    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

Research Projects

 20