x射线成像与光谱学任务(XRISM)上分辨仪器的现状

Y. Ishisaki, R. Kelley, H. Awaki, J. Balleza, K. Barnstable, T. Bialas, R. Boissay-Malaquin, G. Brown, E. Canavan, R. Cumbee, T. Carnahan, M. Chiao, Brian J. Comber, E. Costantini, J. D. den Herder, J. Dercksen, C. D. de Vries, M. Dipirro, M. Eckart, Y. Ezoe, C. Ferrigno, R. Fujimoto, N. Gorter, S. Graham, M. Grim, Leslie S. Hartz, R. Hayakawa, T. Hayashi, N. Hell, A. Hoshino, Y. Ichinohe, M. Ishida, K. Ishikawa, B. James, Steven J. Kenyon, C. Kilbourne, M. Kimball, S. Kitamoto, M. Leutenegger, Y. Maeda, D. McCammon, J. Miko, M. Mizumoto, T. Okajima, A. Okamoto, S. Paltani, F. Porter, Kosuke Sato, Toshiki Sato, M. Sawada, K. Shinozaki, R. Shipman, P. Shirron, G. Sneiderman, Y. Soong, R. Szymkiewicz, A. Szymkowiak, Y. Takei, K. Tamura, M. Tsujimoto, Y. Uchida, S. Wasserzug, M. Witthoeft, Rob Wolfs, S. Yamada, S. Yasuda
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引用次数: 5

摘要

x射线成像和光谱任务(XRISM)上的解析仪器由6 × 6硅热敏电阻微量热计阵列和高通量x射线反射镜组件(XMA)组成,其焦距为5.6 m。XRISM是ASTRO-H/Hitomi的回收任务,Resolve仪器是ASTRO-H软x射线光谱仪(SXS)和软x射线望远镜(SXT)的重建,在轨道上实现了~ 5 eV FWHM的能量分辨率,并根据ASTRO-H的经验进行了一些重要的改变。制作杜瓦和电子盒飞行模型,并于2021年进行仪器测试和校准。通过调整制冷机频率,在6 keV条件下,对于所有36像素和高分辨率事件,能量分辨率优于4.9 eV FWHM,能量尺度精度优于2 eV至30 keV。评价了探测器对微振动、电传导和辐射的抗扰性。该仪器于2022-04年交付给航天器系统,目前正在进行航天器系统测试。XMA分别进行测试和校准。它的角分辨率为1.27 ',镜面本身的有效面积在1 keV时为570 cm2,在6 keV时为424 cm2。我们报告了ASTRO-H SXS的设计和主要变化,集成和仪器测试的结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Status of resolve instrument onboard X-Ray Imaging and Spectroscopy Mission (XRISM)
The resolve instrument onboard the X-Ray Imaging and Spectroscopy Mission (XRISM) consists of an array of 6 × 6 silicon-thermistor microcalorimeters cooled down to 50 mK and a high-throughput x-ray mirror assembly (XMA) with a focal length of 5.6 m. XRISM is a recovery mission of ASTRO-H/Hitomi, and the Resolve instrument is a rebuild of the ASTRO-H soft x-ray spectrometer (SXS) and the Soft X-ray Telescope (SXT) that achieved energy resolution of ∼5 eV FWHM on orbit, with several important changes based on lessons learned from ASTRO-H. The flight models of the Dewar and the electronics boxes were fabricated and the instrument test and calibration were conducted in 2021. By tuning the cryocooler frequencies, energy resolution better than 4.9 eV FWHM at 6 keV was demonstrated for all 36 pixels and high resolution grade events, as well as energy-scale accuracy better than 2 eV up to 30 keV. The immunity of the detectors to microvibration, electrical conduction, and radiation was evaluated. The instrument was delivered to the spacecraft system in 2022-04 and is under the spacecraft system testing as of writing. The XMA was tested and calibrated separately. Its angular resolution is 1.27′ and the effective area of the mirror itself is 570 cm2 at 1 keV and 424 cm2 at 6 keV. We report the design and the major changes from the ASTRO-H SXS, the integration, and the results of the instrument test.
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