Status of Resolve instrument onboard X-Ray Imaging and Spectroscopy Mission (XRISM)

被引：21

作者：

Ishisaki, Yoshitaka ^{[1
,2
]}

Kelley, Richard L. ^{[3
]}

Awaki, Hisamitsu ^{[4
]}

Balleza, Jesus C. ^{[3
]}

Barnstable, Kim R. ^{[3
]}

Bialas, Thomas G. ^{[3
]}

Boissay-Malaquin, Rozenn ^{[3
,5
]}

Brown, Gregory, V ^{[6
]}

Canavan, Edgar R. ^{[3
]}

Cumbee, Renata S. ^{[3
,19
]}

Carnahan, Timothy M. ^{[3
]}

Chiao, Meng P. ^{[3
]}

Comber, Brian J. ^{[3
]}

Costantini, Elisa ^{[7
]}

Den Herder, Jan-Willem A. ^{[7
]}

Dercksen, Johannes ^{[7
]}

de Vries, Cor P. ^{[7
]}

DiPirro, Michael J. ^{[3
]}

Eckart, Megan E. ^{[6
]}

Ezoe, Yuichiro ^{[1
]}

Ferrigno, Carlo ^{[8
]}

Fujimoto, Ryuichi ^{[2
,9
]}

Gorter, Nathalie ^{[7
]}

Graham, Steven M. ^{[3
]}

Grim, Martin ^{[7
]}

Hartz, Leslie S. ^{[3
]}

Hayakawa, Ryota ^{[10
]}

Hayashi, Takayuki ^{[3
,5
]}

Hell, Natalie ^{[6
]}

Hoshino, Akio ^{[11
]}

Ichinohe, Yuto ^{[10
]}

Ishida, Manabu ^{[2
]}

Ishikawa, Kumi ^{[1
]}

James, Bryan L. ^{[3
]}

Kenyon, Steven J. ^{[3
]}

Kilbourne, Caroline A. ^{[3
]}

Kimball, Mark O. ^{[3
]}

Kitamoto, Shunji ^{[10
]}

Leutenegger, Maurice A. ^{[3
]}

Maeda, Yoshitomo ^{[2
]}

McCammon, Dan ^{[12
]}

Miko, Joseph J. ^{[3
]}

Mizumoto, Misaki ^{[13
]}

Okajima, Takashi ^{[3
]}

Okamoto, Atsushi ^{[14
]}

Paltani, Stephane ^{[8
]}

Porter, Frederick S. ^{[3
]}

Sato, Kosuke ^{[15
]}

Sato, Toshiki ^{[10
]}

Sawada, Makoto ^{[16
]}

机构：

[1] Tokyo Metropolitan Univ, Dept Phys, Hachioji, Tokyo 1920397, Japan

[2] JAXA, Inst Space & Astronaut Sci, Chuo Ku, Sagamihara, Kanagawa 2525210, Japan

[3] NASA, Goddard Space Flight Ctr, 8800 Greenbelt Rd, Greenbelt, MD 20771 USA

[4] Ehime Univ, Dept Phys, Matsuyama, Ehime 7908577, Japan

[5] Univ Maryland Baltimore Cty, Ctr Space Sci & Technol, 1000 Hilltop Cir, Baltimore, MD 21250 USA

[6] Lawrence Livermore Natl Lab, 7000 East Ave, Livermore, CA 94550 USA

[7] SRON Netherlands Inst Space Res, Niels Bohrweg 4, NL-2333 CA Leiden, Netherlands

[8] Univ Geneva, Dept Astron, Ch Ec 16, CH-1290 Versoix, Switzerland

[9] Kanazawa Univ, Fac Math & Phys, Kanazawa, Ishikawa 9201192, Japan

[10] Rikkyo Univ, Dept Phys, Toshima Ku, Tokyo 1718501, Japan

[11] JAXA, Inst Space & Astronaut Sci, Tsukuba, Ibaraki 3058505, Japan

[12] Univ Wisconsin, Dept Phys, Madison, WI 53706 USA

[13] Kyoto Univ, Hakubi Ctr, Sakyo Ku, Kyoto 6068501, Japan

[14] JAXA, Res & Dev Directorate, Tsukuba, Ibaraki 3058505, Japan

[15] Saitama Univ, Dept Phys, Sakura Ku, Saitama 3388570, Japan

[16] RIKEN, Cluster Pioneering Res, Wako, Saitama 3510198, Japan

[17] Yale Univ, Yale Ctr Astron & Astrophys, New Haven, CT 06520 USA

[18] Tokyo Univ Sci, Dept Phys, Noda, Chiba 2788510, Japan

[19] Univ Maryland, Dept Astron, College Pk, MD 20742 USA

来源：

SPACE TELESCOPES AND INSTRUMENTATION 2022: ULTRAVIOLET TO GAMMA RAY | 2022年 / 12181卷

关键词：

X-ray; instruments; spectroscopic; microcalorimeter;

D O I：

10.1117/12.2630654

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The Resolve instrument onboard the X-Ray Imaging and Spectroscopy Mission (XRISM) consists of an array of 6 x 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 similar to 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 cm(2) at 1 keV and 424 cm(2) 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.

引用

页数：22

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