Volume 44 Issue 1
Feb.  2024
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Article Navigation >  Chinese Journal of Space Science  > 2024  >  44(1): 178-184 Open Access
ZHANG Xin, XU Wanqiu, BAI Chaoping, SUN Yueqiang, WANG Wenjing, ZHANG Shuai, HAN Jianwei, CHEN Rui, ZHU Xiang, LI Yue. Design and Verification of Multi-detection Unit Based on ASIC Chip (in Chinese). Chinese Journal of Space Science, 2024, 44(1): 178-184 doi: 10.11728/cjss2024.01.2023-0018
Citation: ZHANG Xin, XU Wanqiu, BAI Chaoping, SUN Yueqiang, WANG Wenjing, ZHANG Shuai, HAN Jianwei, CHEN Rui, ZHU Xiang, LI Yue. Design and Verification of Multi-detection Unit Based on ASIC Chip (in Chinese). Chinese Journal of Space Science, 2024, 44(1): 178-184 doi: 10.11728/cjss2024.01.2023-0018
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Design and Verification of Multi-detection Unit Based on ASIC Chip

doi: 10.11728/cjss2024.01.2023-0018 cstr: 32142.14.cjss2024.01.2023-0018
  • 1.

    National Space Science Center, Chinese Academy of Sciences, Beijing 100190

  • 2.

    University of Chinese Academy of Sciences, Beijing 100049

  • Received Date: 2023-02-08
  • Accepted Date: 2023-10-04
  • Rev Recd Date: 2023-04-12
    • Available Online: 2023-08-01
    Abstract
  • Taking particles in space radiation environment as the research background, the space particle detection system using silicon micro-strip sensor as the probe and integrated chip IDE3160 for signal processing is developed. The system is designed by using silicon micro-strip detection array, which is composed of two silicon micro-strip sensors as the front-end probe, and using digital signal processing method to obtain the position of space particle incident and the energy deposited in the unit length (Linear Energy Transfer, LET) in the silicon micro-strip. From the perspective of the physical mechanism inducing single particle effects, the physical effects produced by contrasting heavy ions and pulsed lasers in silicon semiconductors are different. Pulsed laser of 1.064 μm was used to test the system, and good LET linearity results were obtained: The time required for data acquisition is 2.47 ms, the detectable LET threshold is about 0.1 MeV·cm2·mg–1 and the Pearson correlation coefficient is about 0.998, indicating that the system measurement is in good agreement with the theoretical design. The system has a wide dynamic range, good linearity, high integration, scalability and portability, and can be mounted on a variety of space exploration satellites.

     

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