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arXiv 2609.02058astro-ph.IM

基于玻璃编码掩模的轻量软X射线成像仪(LSXI)

Lightweight Soft X-ray Imager (LSXI) with glass-based coded mask

  • State Key Laboratory of Particle Astrophysics, Institute of High Energy Physics(高能物理研究所粒子天体物理国家重点实验室)
  • National Astronomical Observatories, Chinese Academy of Sciences(中国科学院国家天文台)
  • University of Chinese Academy of Sciences(中国科学院大学)
  • TIANFU Cosmic Ray Research Center(天府宇宙线研究中心)
  • School of Materials Science and Engineering,NanChang University(南昌大学材料科学与工程学院)
  • North Night Vision Technology (Nanjing) Research Institute Co.(北方夜视科技(南京)研究院有限公司)
  • School of Physics, Nankai University(南开大学物理学院)

机构由 AI 辅助整理,请以论文原文为准。

Dali Zhang, Chao Zheng, Lu Wang, Haopeng Li, Jinpeng Zhang, Xinqiao Li, Shaolin Xiong, Longhui Li, Zhenghua An, Sheng Yang, Xiaoqing Cong, Zhixing Ling, Hailing… 展开作者

Dali Zhang, Chao Zheng, Lu Wang, Haopeng Li, Jinpeng Zhang, Xinqiao Li, Shaolin Xiong, Longhui Li, Zhenghua An, Sheng Yang, Xiaoqing Cong, Zhixing Ling, Hailing Qin, Xiangyang Wen, Ke Gong, Yaqing Liu, Xiaojing Liu, Xiang Ma, Xiaoyun Zhao, Yanbing Xu, Junhao Yin, Dejun Gong, Jiacong Liu, Chenwei Wang, Min Gao, Jinzhou Wang

AI总结:

本文提出一种基于玻璃微通道板技术的轻量软X射线成像仪,通过X射线束线测量和6U立方卫星的蒙特卡罗模拟验证其适用于空间探测,解决传统编码掩模成像仪体积大、重量重的问题。

AI中文摘要:

编码掩模技术已广泛应用于X射线和伽马射线成像仪,尤其在空间天文学领域。然而,传统编码掩模成像仪的设计通常存在体积大、重量重的问题。本文提出一种基于玻璃微通道板(MCP)技术的新型编码掩模成像仪设计,使其重量控制在1kg以内,兼具紧凑性与自支撑性,非常适合空间探测卫星应用。该设计通过X射线束线测量对编码图案进行重建以完成初步验证,还对集成至6U立方卫星的模块开展蒙特卡罗模拟,评估其在轨探测器性能,包括灵敏度与源定位能力。

英文摘要:

The coded mask technique has been widely used in X-ray and Gamma-ray imagers, especially in space astronomy. However, the traditional design of coded mask imagers usually has problems with large size and heavy weight. Here, we propose a novel design for a coded mask imager made of glass based on microchannel plate (MCP) technology, making it lightweight (within 1 kg), compact, and self-supporting, which is very suitable for space exploration satellites. The design is initially demonstrated by reconstructing encoded patterns from measurements at the X-ray beamline. Monte Carlo simulations of the module integrated into a 6U CubeSat are conducted to assess its in-orbit detector performance, including sensitivity and source localization.

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