論文

査読有り
2016年

The Astro-H high resolution soft X-ray spectrometer

Proceedings of SPIE - The International Society for Optical Engineering
  • Richard L. Kelley
  • Hiroki Akamatsu
  • Phillipp Azzarell
  • Tom Bialas
  • Kevin R. Boyce
  • Gregory V. Brown
  • Edgar Canavan
  • Meng P. Chiao
  • Elisa Costantini
  • Michael J. DiPirro
  • Megan E. Eckart
  • Yuichiro Ezoe
  • Ryuichi Fujimoto
  • Daniel Haas
  • Jan-Willem Den Herder
  • Akio Hoshino
  • Kumi Ishikawa
  • Yoshitaka Ishisaki
  • Naoko Iyomoto
  • Caroline A. Kilbourne
  • Mark Kimball
  • Shunji Kitamoto
  • Saori Konami
  • Shu Koyama
  • Maurice A. Leutenegger
  • Dan McCammon
  • Joseph Miko
  • Kazuhisa Mitsuda
  • Ikuyuki Mitsuishi
  • Harvey Moseley
  • Hiroshi Murakami
  • Masahide Murakami
  • Hirofumi Noda
  • Mina Ogawa
  • Takaya Ohashi
  • Atsushi Okamoto
  • Naomi Ota
  • Stéphane Paltani
  • F. Scott Porter
  • Kazuhiro Sakai
  • Kosuke Sato
  • Yohichi Sato
  • Makoto Sawada
  • Hiromi Seta
  • Keisuke Shinozaki
  • Peter J. Shirron
  • Gary A. Sneiderman
  • Hiroyuki Sugita
  • Andrew E. Szymkowiak
  • Yoh Takei
  • Toru Tamagawa
  • Makoto Tashiro
  • Yukikatsu Terada
  • Masahiro Tsujimoto
  • Cor P. De Vries
  • Shinya Yamada
  • Noriko Y. Yamasaki
  • Yoichi Yatsu
  • 全て表示

9905
記述言語
英語
掲載種別
研究論文(国際会議プロシーディングス)
DOI
10.1117/12.2232509
出版者・発行元
SPIE

We present the overall design and performance of the Astro-H (Hitomi) Soft X-Ray Spectrometer (SXS). The instrument uses a 36-pixel array of x-ray microcalorimeters at the focus of a grazing-incidence x-ray mirror Soft X-Ray Telescope (SXT) for high-resolution spectroscopy of celestial x-ray sources. The instrument was designed to achieve an energy resolution better than 7 eV over the 0.3-12 keV energy range and operate for more than 3 years in orbit. The actual energy resolution of the instrument is 4-5 eV as demonstrated during extensive ground testing prior to launch and in orbit. The measured mass flow rate of the liquid helium cryogen and initial fill level at launch predict a lifetime of more than 4 years assuming steady mechanical cooler performance. Cryogen-free operation was successfully demonstrated prior to launch. The successful operation of the SXS in orbit, including the first observations of the velocity structure of the Perseus cluster of galaxies, demonstrates the viability and power of this technology as a tool for astrophysics.

リンク情報
DOI
https://doi.org/10.1117/12.2232509
Web of Science
https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=JSTA_CEL&SrcApp=J_Gate_JST&DestLinkType=FullRecord&KeyUT=WOS:000387731500020&DestApp=WOS_CPL
ID情報
  • DOI : 10.1117/12.2232509
  • ISSN : 1996-756X
  • ISSN : 0277-786X
  • SCOPUS ID : 85003530545
  • Web of Science ID : WOS:000387731500020

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