研究者業績

金丸 善朗

カネマル ヨシアキ  (Yoshiaki Kanemaru)

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 宇宙航空プロジェクト研究員
学位
博士(工学)(宮崎大学)

ORCID ID
 https://orcid.org/0000-0002-4541-1044
J-GLOBAL ID
202301012755167955
researchmap会員ID
R000052242

受賞

 1

論文

 15
  • Hiromasa Suzuki, Tomokage Yoneyama, Shogo B. Kobayashi, Hirofumi Noda, Hiroyuki Uchida, Kumiko K. Nobukawa, Kouichi Hagino, Koji Mori, Hiroshi Tomida, Hiroshi Nakajima, Takaaki Tanaka, Hiroshi Murakami, Hideki Uchiyama, Masayoshi Nobukawa, Yoshiaki Kanemaru, Yoshinori Otsuka, Haruhiko Yokosu, Wakana Yonemaru, Hanako Nakano, Kazuhiro Ichikawa, Reo Takemoto, Tsukasa Matsushima, Marina Yoshimoto, Mio Aoyagi, Kohei Shima, Yuma Aoki, Yamato Ito, Kaito Fukuda, Honoka Kiyama, Daiki Aoki, Kaito Fujisawa, Yasuyuki Shimizu, Mayu Higuchi, Masahiro Fukuda, Natsuki Sakamoto, Ryuichi Azuma, Shun Inoue, Takayoshi Kohmura, Makoto Yamauchi, Isamu Hatsukade, Hironori Matsumoto, Hirokazu Odaka, Tsunefumi Mizuno, Tessei Yoshida, Yoshitomo Maeda, Manabu Ishida, Takeshi Go Tsuru, Kazutaka Yamaoka, Takashi Okajima, Takayuki Hayashi, Junko S. Hiraga, Masanobu Ozaki, Tadayasu Dotani, Hiroshi Tsunemi, Kiyoshi Hayashida
    Space Telescopes and Instrumentation 2024: Ultraviolet to Gamma Ray 228-228 2024年8月21日  
  • Katsuhiro Hayashi, Makoto S. Tashiro, Yukikatsu Terada, Tessei Yoshida, Shoji Ogawa, Yoshiaki Kanemaru, Kotaro Fukushima, Akio Hoshino, Hiromitsu Takahashi, Masayoshi Nobukawa, Tsunefumi Mizuno, Kazuhiro Nakazawa, Shin'ichiro Uno, Ken Ebisawa, Satoshi Eguchi, Satoru Katsuda, Takao Kitaguchi, Aya Kubota, Naomi Ota, Megumi Shidatsu, Atsushi Tanimoto, Yuichi Terashima, Yohko Tsuboi, Yuusuke Uchida, Hideki Uchiyama, Shigeo Yamauchi, Tomokage Yoneyama, Satoshi Yamada, Nagomi Uchida, Seiko Sakurai, Shin Watanabe, Ryo Iizuka, Rie Sato, Chris Baluta, Takayuki Tamura, Yasushi Fukazawa, Hirokazu Odaka, Tsubasa Tamba, Ryohei Sato, Sou Kato, Minami Sakama, Takumi Shioiri, Yuki Niida, Natsuki Sakamoto, Noboru Nemoto, Yuki Omiya, Nari Suzuki, Toshihiro Takagi, Yugo Motogami, Matt Holland, Michael Loewenstein, Eric D. Miller, Tahir Yaqoob, Robert S. Hill, Trisha F. Doyle, Efrain Perez-Solis, Morgan D. Waddy, Mark Mekosh, Joseph B. Fox, Matteo Guainazzi, Jan-Uwe Ness, Hironori Maejima, Kenichi Toda, Chikara Natsukari
    Space Telescopes and Instrumentation 2024: Ultraviolet to Gamma Ray 60-60 2024年8月21日  
  • Yohko Tsuboi, Koichiro Akasu, Noboru Nemoto, Tomokage Yoneyama, Marina Yoshimoto, Kotaro Fukushima, Katsuhiro Hayashi, Yoshiaki Kanemaru, Shoji Ogawa, Tessei Yoshida, Marc Audard, Ehud Behar, Shun Inoue, Yuiko Ishihara, Takayoshi Komura, Yoshitomo Maeda, Misaki Mizumoto, Masayoshi Nobukawa, Katja Pottschmidt, Megumi Shidatsu, Yukikatsu Terada, Yuichi Terashima, Hiroyuki Uchida
    Space Telescopes and Instrumentation 2024: Ultraviolet to Gamma Ray 236-236 2024年8月21日  
  • Hirofumi Noda, Mio Aoyagi, Koji Mori, Hiroshi Tomida, Hiroshi Nakajima, Takaaki Tanaka, Hiromasa Suzuki, Hiroshi Murakami, Hiroyuki Uchida, Takeshi Go Tsuru, Keitaro Miyazaki, Kohei Kusunoki, Yoshiaki Kanemaru, Yuma Aoki, Kumiko K. Nobukawa, Masayoshi Nobukawa, Kohei Shima, Marina Yoshimoto, Kazunori Asakura, Hironori Matsumoto, Tomokage Yoneyama, Shogo B. Kobayashi, Kouichi Hagino, Hideki Uchiyama, Kiyoshi Hayashida
    Space Telescopes and Instrumentation 2024: Ultraviolet to Gamma Ray 226-226 2024年8月21日  
  • Yuma Aoki, Yamato Ito, Masayoshi Nobukawa, Yoshiaki Kanemaru, Keitaro Miyazaki, Kohei Kusunoki, Koji Mori, Tomokage Yoneyama, Tsubasa Tamba, Hiroshi Tomida, Hiroshi Nakajima, Hironori Matsumoto, Hirofumi Noda, Kiyoshi Hayashida, Hiroyuki Uchida, Takaaki Tanaka, Hiromasa Suzuki, Tessei Yoshida, Hiroshi Murakami, Makoto Yamauchi, Isamu Hatsukade, Kouichi Hagino, Takayoshi Kohmura, Hideki Uchiyama, Kazutaka Yamaoka, Masanobu Ozaki, Tadayasu Dotani, Hiroshi Tsunemi, Kumiko Nobukawa, Takeshi Tsuru, Shogo Kobayashi, Junko Hiraga
    Proceedings of 10th International Workshop on Semiconductor Pixel Detectors for Particles and Imaging — PoS(Pixel2022) 2023年3月16日  
  • Koji Mori, Hiroshi Tomida, Hiroshi Nakajima, Takashi Okajima, Hirofumi Noda, Takaaki Tanaka, Hiroyuki Uchida, Kouichi Hagino, Shogo Benjamin Kobayashi, Hiromasa Suzuki, Tessei Yoshida, Hiroshi Murakami, Hideki Uchiyama, Masayoshi Nobukawa, Kumiko Nobukawa, Tomokage Yoneyama, Hironori Matsumoto, Takeshi Tsuru, Makoto Yamauchi, Isamu Hatsukade, Manabu Ishida, Yoshitomo Maeda, Takayuki Hayashi, Keisuke Tamura, Rozenn Boissay-Malaquin, Toshiki Sato, Junko Hiraga, Takayoshi Kohmura, Kazutaka Yamaoka, Tadayasu Dotani, Masanobu Ozaki, Hiroshi Tsunemi, Yoshiaki Kanemaru, Jin Sato, Toshiyuki Takaki, Yuta Terada, Keitaro Miyazaki, Kohei Kusunoki, Yoshinori Otsuka, Haruhiko Yokosu, Wakana Yonemaru, Yoh Asahina, Kazunori Asakura, Marina Yoshimoto, Yuichi Ode, Junya Sato, Tomohiro Hakamata, Mio Aoyagi, Yuma Aoki, Shun Tsunomachi, Toshiki Doi, Daiki Aoki, Kaito Fujisawa, Masatoshi Kitajima, Kiyoshi Hayashida
    Proceedings of SPIE - The International Society for Optical Engineering 12181 2022年  
    Xtend is a soft x-ray imaging telescope developed for the x-ray imaging and spectroscopy mission (XRISM). XRISM is scheduled to be launched in the Japanese fiscal year 2022. Xtend consists of the soft x-ray imager (SXI), an x-ray CCD camera, and the x-ray mirror assembly (XMA), a thin-foil-nested conically approximated Wolter-I optics. The SXI uses the P-channel, back-illuminated type CCD with an imaging area size of 31mm on a side. The four CCD chips are arranged in a 2×2 grid and can be cooled down to -120 °C with a single-stage Stirling cooler. The XMA nests thin aluminum foils coated with gold in a confocal way with an outer diameter of 45 cm. A pre-collimator is installed in front of the x-ray mirror for the reduction of the stray light. Combining the SXI and XMA with a focal length of 5.6m, a field of view of 38′ × 38′ over the energy range from 0.4 to 13 keV is realized. We have completed the fabrication of the flight model of both SXI and XMA. The performance verification has been successfully conducted in a series of sub-system level tests. We also carried out on-ground calibration measurements and the data analysis is ongoing.
  • Tomokage Yoneyama, Hirofumi Noda, Maho Hanaoka, Koki Okazaki, Kazunori Asakura, Kiyoshi Hayashida, Ayami Ishikura, Shotaro Sakuma, Kengo Hattori, Hironori Matsumoto, Koji Mori, Yoshiaki Kanemaru, Jin Sato, Toshiyuki Takaki, Hiroyuki Uchida, Takaaki Tanaka, Hiromichi Okon, Yuki Amano, Takeshi G. Tsuru, Hiroshi Tomida, Junko S. Hiraga, Yukino Urabe, Kumiko K. Nobukawa, Mariko Saito, Masayoshi Nobukawa, Takashi Sako, Hideki Uchiyama, Hiroshi Nakajima, Akira Kashimura, Shogo B. Kobayashi, Kouichi Hagino, Hiroshi Murakami
    Nuclear Instruments and Methods in Physics Research, Section A: Accelerators, Spectrometers, Detectors and Associated Equipment 985 2021年1月1日  
    X-ray Imaging Spectroscopy Mission (XRISM) is the next Japanese X-ray astronomical satellite to be launched in 2021 Japanese fiscal year. We are developing one of the XRISM instruments “Xtend”, which is an X-ray CCD camera combined with an X-ray telescope, and achieves the wide field of view of 38′×38′ in 0.4–13keV. In 2019, twelve flight-model (FM) candidate CCD chips were fabricated by Hamamatsu Photonics K.K. We conducted screening experiments to examine whether the FM candidates met requirements for the Xtend CCDs, and selected the four FM chips from them. We constructed a screening system, with which we can examine various CCD performances by illuminating characteristic X-ray lines in a ∼0.5–14keV band or optical lights. With this system, all the twelve candidates were confirmed to satisfy the requirements. We then selected four chips with the best performance, in terms of e.g., their charge transfer inefficiencies, energy resolutions, soft X-ray sensitivities, and optical light leakages. In this paper, we report an overview of the screening system, and procedures and results of the screening process.
  • Yoshiaki Kanemaru, Jin Sato, Toshiyuki Takaki, Yuta Terada, Koji Mori, Mariko Saito, Kumiko K. Nobukawa, Takaaki Tanaka, Hiroyuki Uchida, Kiyoshi Hayashida, Hironori Matsumoto, Hirofumi Noda, Maho Hanaoka, Tomokage Yoneyama, Koki Okazaki, Kazunori Asakura, Shotaro Sakuma, Kengo Hattori, Ayami Ishikura, Yuki Amano, Hiromichi Okon, Takeshi G. Tsuru, Hiroshi Tomida, Hikari Kashimura, Hiroshi Nakajima, Takayoshi Kohmura, Kouichi Hagino, Hiroshi Murakami, Shogo B. Kobayashi, Yusuke Nishioka, Makoto Yamauchi, Isamu Hatsukade, Takashi Sako, Masayoshi Nobukawa, Yukino Urabe, Junko S. Hiraga, Hideki Uchiyama, Kazutaka Yamaoka, Masanobu Ozaki, Tadayasu Dotani, Hiroshi Tsunemi
    Nuclear Instruments and Methods in Physics Research, Section A: Accelerators, Spectrometers, Detectors and Associated Equipment 984 2020年12月21日  
    We present experimental studies on the charge transfer inefficiency (CTI) of charge-coupled device (CCD) developed for the soft X-ray imaging telescope, Xtend, aboard the XRISM satellite. The CCD is equipped with a charge injection (CI) capability, in which sacrificial charge is periodically injected to fill the charge traps. By evaluating the re-emission of the trapped charge observed behind the CI rows, we find that there are at least three trap populations with different time constants. The traps with the shortest time constant, which is equivalent to a transfer time of approximately one pixel, are mainly responsible for the trailing charge of an X-ray event seen in the following pixel. A comparison of the trailing charge in two clocking modes reveals that the CTI depends not only on the transfer time but also on the area, namely the imaging or storage area. We construct a new CTI model by taking into account both transfer-time and area dependence. This model reproduces the data obtained in both clocking modes consistently. We also examine apparent flux dependence of the CTI observed without the CI technique. The higher incident X-ray flux is, the lower the CTI value becomes. It is due to a sacrificial charge effect by another X-ray photon. This effect is found to be negligible when the CI technique is used.
  • A. Takeda, K. Mori, Y. Nishioka, T. Hida, M. Yukumoto, Y. Kanemaru, S. Yonemura, K. Mieda, T. G. Tsuru, T. Tanaka, I. Kurachi, Y. Arai
    Journal of Instrumentation 15(12) 2020年12月  
    This paper reports on the development of on-chip pattern processing in the event-driven silicon-on-insulator pixel detector for X-ray astronomy with background rejection purpose. X-ray charge-coupled device (CCD) detectors, well-established pixel detectors used in this field, has proven that classification of detected events considering their spatial pattern is effective for particle background rejection. Based on the current architecture of our device and from the CCD images obtained in space, we first established a design concept and algorithm of the pattern processor to be implemented. Then, we developed a new device, including a prototype pattern-processing circuit. Experiments using X-ray and beta-ray radioisotopes demonstrated that the pattern processor properly works as expected, and the particle background rejection is realized in an on-chip fashion. This function is useful, especially in a limited-resource system such as the CubeSat.
  • Hiroyuki Uchida, Takaaki Tanaka, Yuki Amano, Hiromichi Okon, Takeshi G. Tsuru, Hiroshi Nakajima, Hirofumi Noda, Kiyoshi Hayashida, Hironori Matsumoto, Maho Hanaoka, Tomokage Yoneyama, Koki Okazaki, Kazunori Asakura, Shotaro Sakuma, Kengo Hattori, Ayami Ishikura, Mariko Saito, Kumiko K. Nobukawa, Hiroshi Tomida, Yoshiaki Kanemaru, Jin Sato, Toshiyuki Takaki, Yuta Terada, Koji Mori, Hikari Kashimura, Takayoshi Kohmura, Kouichi Hagino, Hiroshi Murakami, Shogo B. Kobayashi, Yusuke Nishioka, Makoto Yamauchi, Isamu Hatsukade, Takashi Sako, Masayoshi Nobukawa, Yukino Urabe, Junko S. Hiraga, Hideki Uchiyama, Kazutaka Yamaoka, Masanobu Ozaki, Tadayasu Dotani, Hiroshi Tsunemi, Hisanori Suzuki, Shin ichiro Takagi, Kenichi Sugimoto, Sho Atsumi, Fumiya Tanaka
    Nuclear Instruments and Methods in Physics Research, Section A: Accelerators, Spectrometers, Detectors and Associated Equipment 978 2020年10月21日  
    We have been developing P-channel Charge-Coupled Devices (CCDs) for the upcoming X-ray Astronomy Satellite XRISM, planned to be launched in 2021. While the basic design of the CCD camera (Soft X-ray Imager: SXI) is almost the same as that of the lost Hitomi (ASTRO-H) observatory, we are planning to reduce the phenomenon of “light leakages” that is one of the largest problems recognized in Hitomi data. We adopted a double-layer optical blocking layer on the XRISM CCDs and also added an extra aluminum layer on the backside of them. We develop a newly designed test sample CCD and irradiate it with optical light to evaluate the optical blocking performance. As a result, light leakages are effectively reduced compared with that of the Hitomi CCDs. We thus conclude that the issue is solved by the new design and that the XRISM CCDs satisfy the mission requirement for the SXI.
  • Satoru Katsuda, Masanori Ohno, Koji Mori, Tatsuhiko Beppu, Yoshiaki Kanemaru, Makoto S. Tashiro, Yukikatsu Terada, Kosuke Sato, Kae Morita, Hikari Sagara, Futa Ogawa, Haruya Takahashi, Hiroshi Murakami, Masayoshi Nobukawa, Hiroshi Tsunemi, Kiyoshi Hayashida, Hironori Matsumoto, Hirofumi Noda, Hiroshi Nakajima, Yuichiro Ezoe, Yohko Tsuboi, Yoshitomo Maeda, Takaaki Yokoyama, Noriyuki Narukage
    Astrophysical Journal 891(2) 2020年3月10日  
    We report X-ray spectroscopic results for four giant solar flares that occurred on 2005 September 7 (X17.0), 2005 September 8 (X5.4), 2005 September 9 (X6.2), and 2006 December 5 (X9.0), obtained from Earth albedo data with the X-ray Imaging Spectrometer (XIS) on board Suzaku. The good energy resolution of the XIS (FWHM ∼ 100 eV) enables us to separate a number of line-like features and detect the underlying continuum emission. These features include Si Heα, Si Lyα, S Heα, S Lyα, Ar Heα, and Ca Heα originating from solar flares as well as fluorescent Ar Kα and Ar Kβ from the Earth's atmosphere. Absolute elemental abundances (X/H) averaged over the four flares are obtained to be ∼2.0 (Ca), ∼0.7 (Si), ∼0.3 (S), and ∼0.9 (Ar) at around flare peaks. This abundance pattern is similar to those of active stars' coronae showing inverse first ionization potential (i-FIP) effects, i.e., elemental abundances decrease with decreasing FIP with a turnover at the low end of the FIP. The abundances are almost constant during the flares, with the exception of Si which increases by a factor of ∼2 in the decay phase. The evolution of the Si abundance is consistent with the finding that the i-FIP plasma originates from chromospheric evaporation and then mixes with the surrounding low-FIP biased materials. Flare-to-flare abundance varied by a factor of two, agreeing with past observations of solar flares. Finally, we emphasize that Earth albedo data acquired by X-ray astronomy satellites like Suzaku and the X-Ray Imaging Spectroscopy Mission can significantly contribute to studies of solar physics.
  • Hiroshi Nakajima, Kiyoshi Hayashida, Hiroshi Tomida, Koji Mori, Hirofumi Noda, Hironori Matsumoto, Tomokage Yoneyama, Koki Okazaki, Kazunori Asakura, Maho Hanaoka, Kengo Hattori, Ayami Ishikura, Shotaro Sakuma, Takaaki Tanaka, Hiroyuki Uchida, Takeshi Tsuru, Yuki Amano, Hiromichi Okon, Makoto Yamauchi, Isamu Hatsukade, Yusuke Nishioka, Yoshiaki Kanemaru, Jin Sato, Toshiyuki Takaki, Yuta Terada, Tessei Yoshida, Takayoshi Kohmura, Kouichi Hagino, Shogo Kobayashi, Hiroshi Murakami, Hikari Kashimura, Hideki Uchiyama, Kazutaka Yamaoka, Masayoshi Nobukawa, Takashi Sako, Kumiko Nobukawa, Mariko Saito, Junko Hiraga, Yukino Urabe, Masayuki Yoshida, Tadayasu Dotani, Masanobu Ozaki, Hiroshi Tsunemi
    Proceedings of SPIE - The International Society for Optical Engineering 11444 2020年  
    Soft X-ray Imager (SXI) is the X-ray CCD camera onboard X-Ray Imaging and Spectroscopy Mission (XRISM) that is scheduled to be launched in Japanese fiscal year 2022. Combining the SXI with an X-ray mirror assembly, we realize the Soft X-ray Imaging Telescope (Xtend) with a focal length of 5.6 m and a field of view of 38 arcmin square. The high quantum efficiency of the focal-plane sensor, P-channel back-illumination type CCD, brings about the wide effective energy range from 0.4 to 13 keV with moderate energy resolution. Although the design of the SXI for XRISM is basically identical to that for Hitomi satellite, we have applied several improvements to the CCDs in terms of the charge transfer inefficiency (CTI) and the optical blocking performance. For the former issue, we introduce a notch implant in the charge transfer path to reduce the CTI increase in orbit. For the latter, we change the design of aluminum layers on the incident surface of the CCDs to decrease incoming visible light and/or infrared. Four flight model (FM) CCDs have been selected considering several items including energy resolution at 5.9 keV, CTI, dark current, etc. We have also completed calibration campaign for all the FM CCDs. Initial analyses show that the response function for monochromatic X-rays is basically the same as that of Hitomi CCDs. Front-end ASIC have been confirmed to properly function even after the long-term storage after the manufacture for Hitomi SXI. Then the analog electronics for driving CCDs and for processing the output analog signals have been implemented. Their functional tests have been completed with no problem. The focal plane including the single-stage Stirling cooler has been assembled. Production of key parts in SXI sensor body such as contamination blocking filter and onboard calibration source has been finished and they are waiting for assemble. The digitized signals of the CCD are corrected step by step before conversion to X-ray energy. We are preparing calibration database for the correction such as CTI, gain, and line redistribution function.
  • Tomokage Yoneyama, Hirofumi Noda, Maho Hanaoka, Kiyoshi Hayashida, Koki Okazaki, Kazunori Asakura, Yoshiaki Kanemaru, Jin Sato, Toshiyuki Takaki, Koji Mori, Takashi Sako, Masayoshi Nobukawa, Mariko Saito, Kumiko K. Nobukawa, Hiroshi Murakami, Yuki Amano, Hiroyuki Uchida, Hideki Uchiyama, Hiroshi Tomida, Hiroshi Nakajima, Kengo Hattori, Shotaro Sakuma, Ayami Ishikura, Hironori Matsumoto, Hiromichi Okon, Takaaki Tanaka, Takeshi G. Tsuru, Yukino Urabe, Junko S. Hiraga, Akira Kashimura, Shogo B. Kobayashi, Kouichi Hagino
    Proceedings of SPIE - The International Society for Optical Engineering 11444 2020年  
    X-Ray Imaging and Spectroscopy Mission (XRISM) is the seventh Japanese X-ray astronomical satellite scheduled to be launched in the Japanese fiscal year 2022. XRISM has two mission instruments, “Resolve”, a soft X-ray spectrometer, and “Xtend”, a soft X-ray imager. The Former is an X-ray micro-calorimeter that has ∼ 5 eV of energy resolution with 3′ × 3′ of field of view. The Latter is an X-ray CCD camera with 38′ × 38′ of field of view. Both instruments are placed on the focal plane of X-ray telescopes, X-ray Mirror Assembly (XMA). Xtend CCDs are designed almost the same as those of Hitomi (ASTRO-H), whereas some improvements have been applied. In 2019, flight-model (FM) candidates of Xtend CCDs were fabricated by Hamamatsu Photonics K.K. We performed screening experiments to examine whether they met requirements or not, and then selected the best four chips as the FM. We then performed on-ground calibration on August 2019 and September 2019 for the FM chips to determine the gain correction parameters and to construct the detector response with several energies of monochromatic X-ray. In this paper, we report screening, selection, and on-ground calibration processes, especially focusing on the response verification.
  • Y. Kanemaru, J. Sato, K. Mori, H. Nakajima, Y. Nishioka, A. Takeda, K. Hayashida, H. Matsumoto, J. Iwagaki, K. Okazaki, K. Asakura, T. Yoneyama, H. Uchida, H. Okon, T. Tanaka, T. G. Tsuru, H. Tomida, T. Shimoi, T. Kohmura, K. Hagino, H. Murakami, S. B. Kobayashi, M. Yamauchi, I. Hatsukade, M. Nobukawa, K. K. Nobukawa, J. S. Hiraga, H. Uchiyama, K. Yamaoka, M. Ozaki, T. Dotani, H. Tsunemi, T. Hamano
    Journal of Instrumentation 14(4) 2019年4月  
    We report the radiation hardness of a p-channel CCD developed for the X-ray CCD camera onboard the XRISM satellite. This CCD has basically the same characteristics as the one used in the previous Hitomi satellite, but newly employs a notch structure of potential for signal charges by increasing the implant concentration in the channel . The new device was exposed up to approximately 7.9 × 1010 protons cm-2 at 100 MeV . The charge transfer inefficiency was estimated as a function of proton fluence with an 55Fe source. A device without the notch structure was also examined for comparison. The result shows that the notch device has a significantly higher radiation hardness than those without the notch structure including the device adopted for Hitomi. This proves that the new CCD is radiation tolerant for space applications with a sufficient margin.
  • Kiyoshi Hayashida, Hiroshi Tomida, Koji Mori, Hiroshi Nakajima, Takaaki Tanaka, Hiroyuki Uchida, Takeshi G. Tsuru, Hiroshi Murakami, Takashi Okajima, Takayoshi Kohmura, Kouichi Hagino, Shogo B. Kobayashi, Manabu Ishida, Yoshitomo Maeda, Hideki Uchiyama, Kazutaka Yamaoka, Hironori Matsumoto, Masayoshi Nobukawa, Kumiko K. Nobukawa, Junko S. Hiraga, Makoto Yamauchi, Isamu Hatsukade, Yang Soong, Hideyuki Mori, Takayuki Hayashi, Hiroshi Tsunemi, Masanobu Ozaki, Tadayasu Dotani, Junichi Iwagaki, Tomokage Yoneyama, Koki Okazaki, Kazunori Asakura, Satomi Onishi, Yoshiaki Kanemaru, Jin Sato, Yusuke Nishioka, Ayaki Takeda, Hiromichi Okon, Masayuki Yoshida, Takeo Shimoi
    Proceedings of SPIE - The International Society for Optical Engineering 10699 2018年  
    X-ray Astronomy Recovery Mission (XARM) scheduled to be launched in early 2020's carries two soft X-ray telescopes. One is Resolve consisting of a soft X-ray mirror and a micro calorimeter array, and the other is Soft X-ray Imaging Telescope (Xtend), a combination of an X-ray mirror assembly (XMA) and an X-ray CCD camera (SXI). Xtend covers a field of view (FOV) of 38′ × 38′, much larger than that of Resolve (3′ × 3 ′) with moderate energy resolution in the energy band from 0.4 keV to 13 keV, which is similar to that of Resolve (from 0.3 keV to 12 keV). Simultaneous observations of both telescopes provide complimentary data of X-ray sources in their FOV. In particular, monitoring X-ray sources outside the Resolve FOV but inside the Xtend FOV is important to enhance the reliability of super high resolution spectra obtained with Resolve. Xtend is also expected to be one of the best instruments for low surface brightness X-ray emissions with its low non X-ray background level, which is comparable to that of Suzaku XIS. The design of Xtend is almost identical to those of Soft X-ray Telescope (SXT) and Soft X-ray Imager (SXI) both on board the Hitomi satellite. However, several mandatory updates are included. Updates for the CCD chips are verified with experiment using test CCD chips before finalizing the design of the flight model CCD. Fabrication of the foils for XMA has started, and flight model production of the SXI is almost ready.

MISC

 11
  • 青木悠馬, 伊藤耶馬斗, 福田開大, 木山穂乃香, 信川久実子, 信川正順, 森浩二, 冨田洋, 中嶋大, 野田博文, 鈴木寛大, 小林翔悟, 萩野浩一, 内田裕之, 米山友景, 田中孝明, 村上弘志, 幸村孝由, 鶴剛, 松本浩典, 小高裕和, 山内誠, 廿日出勇, 山岡和貴, 内山秀樹, 吉田鉄生, 金丸善朗, 水野恒史
    日本天文学会年会講演予稿集 2024 2024年  
  • 信川久美子, 森浩二, 森浩二, 冨田洋, 中嶋大, 中嶋大, 野田博文, 林田清, 鈴木寛大, 小林翔悟, 内田裕之, 萩野浩一, 青木悠馬, 伊藤耶馬斗, 金丸善朗, 宮崎啓太郎, 楠康平, 大塚芳徳, 横須晴彦, 米丸若菜, 市川雄大, 中野瑛子, 中村彰太郎, 亀井貴光, 朝倉一統, 善本真梨那, 大出優一, 佐藤淳矢, 袴田知宏, 青柳美緒, 角町駿, 土居俊輝, 青木大輝, 藤澤海斗, 清水康行, 畠中大介, 田中孝明, 村上弘志, 信川正順, 内山秀樹, 吉田鉄生, 米山友景, 幸村孝由, 鶴剛, 松本浩典, OKAJIMA Takashi, 石田学, 前田良知, 山内誠, 廿日出勇, 平賀純子, 山岡和貴, 尾崎正伸, 堂谷忠靖, 常深博
    日本天文学会年会講演予稿集 2023 2023年  
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共同研究・競争的資金等の研究課題

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