Preflight performance of the ASTRO-E hard-x-ray detector

التفاصيل البيبلوغرافية
العنوان: Preflight performance of the ASTRO-E hard-x-ray detector
المؤلفون: Chiharu Tanihata, Jun Kataoka, Toshio Murakami, Naomi Ota, Hideki Ozawa, Tadayuki Takahashi, Takayuki Tamura, Yasunobu Uchiyama, S. Watanabe, Kazutaka Yamaoka, D. Yonetoku, Y. Ezoe, Yasushi Fukazawa, Naoki Isobe, Naoko Iyomoto, Tuneyoshi Kamae, Motohide Kokubun, J. Kotoku, Aya Kubota, Kazuo Makishima, Yukari Matsumoto, Tsunefumi Mizuno, Kazuhiro Nakazawa, Tomohisa Onishi, Masahiko Sugiho, Ikuya Takahashi, Masaaki Tanaka, Makoto Tashiro, Yukikatsu Terada, Masaharu Nomachi, Atsumasa Yoshida, M. Hamaya, M. Horii, Koji Taguchi, N. Morita, I. Odagi, Kunihiko Sato, Y. Tanaka, Kunishiro Mori
المصدر: SPIE Proceedings.
بيانات النشر: SPIE, 1999.
سنة النشر: 1999
مصطلحات موضوعية: Physics, Photomultiplier, Optics, business.industry, Optical engineering, Detector, Orbit (dynamics), X-ray detector, Calibration, Satellite, Orbital mechanics, business
الوصف: The hard x-ray detector (HXD) is one of the three experiments of the Astro-E mission, the fifth Japanese X-ray Satellite devoted to studies of high energy phenomena in the universe in the x-ray to soft gamma-ray region. Prepared for launch at the beginning of 200 via the newly developed M-V launch vehicle of the Institute of Space and Astronomical Science, the Astro-E is to be thrown in to a near-circular orbit of 550 km altitude, with an inclination of 31 degrees. The flight model has been finished assembled this year, and we carried out various tests to verify the performance. We acquired the background spectrum at sea level, and confirmed that our system is operating effectively in reducing the background level. The HXD will observe photons in the energy range of 10-600 keV, and the calculations based on the preflight calibration suggest that the HXD will have the highest sensitivity ever achieved in this energy range. We also verified that our electronic system will maintain its performance against charged particle events expected in orbit.© (1999) COPYRIGHT SPIE--The International Society for Optical Engineering. Downloading of the abstract is permitted for personal use only.
تدمد: 0277-786X
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::11e63298df9dbe167b0d3c9b328f4e8a
https://doi.org/10.1117/12.366546
حقوق: OPEN
رقم الأكسشن: edsair.doi...........11e63298df9dbe167b0d3c9b328f4e8a
قاعدة البيانات: OpenAIRE