Ground testing and calibration of focal plane detector flight model on board the first pathfinder of CATCH

CATCH -1, as the first satellite of Chasing All Transients Constellation Hunters ( CATCH ) space mission, was successfully launched into its expected orbit on June 22, 2024. The flight model underwent environmental tests before launch, including thermal cycling, thermal vacuum, and mechanical evalua...

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Published inExperimental astronomy Vol. 59; no. 1
Main Authors Li, Panping, Zhao, Kang, Wen, Xiangyang, Li, Zhengwei, Gao, Min, Yin, Qian-Qing, Tao, Lian, Zhao, Qingchang, Wang, Yusa, Zhao, Zijian, Zhao, Shujie, Huang, Yiming, Xiao, Jingyu, Zhang, Yifan, Meng, Bin, Yang, Sheng, Chen, Wen, Zhou, Heng, Yang, Yong, He, Huilin, Ma, Ruican, Yang, Shuai, Huang, Guoli, Li, YaJun, Cao, Jiewei, Hou, Shu-Jin, Liu, Xiaojing, Wang, Jinzhou, Sun, Liang, Zhang, Shuang-Nan, Xiong, Shaolin, Ma, Xiang, Huang, Yue, Song, Liming
Format Journal Article
LanguageEnglish
Published Dordrecht Springer Netherlands 01.02.2025
Springer Nature B.V
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Abstract CATCH -1, as the first satellite of Chasing All Transients Constellation Hunters ( CATCH ) space mission, was successfully launched into its expected orbit on June 22, 2024. The flight model underwent environmental tests before launch, including thermal cycling, thermal vacuum, and mechanical evaluations. The CATCH -1 detector system is equipped with a 4-pixel Silicon Drift Detector (SDD) array. To ensure the reliability and redundancy of the CATCH -1 detector system, two sets of data acquisition systems were independently designed and calibrated. Our focus is on presenting the ground calibration results of CATCH -1, which demonstrate a strong linear correlation between energy and channel. The main data acquisition system achieves an energy resolution of ∼ 120 eV@4 keV, while the backup data acquisition system has a slightly lower energy resolution of around 150 eV@4 keV, both meeting the design requirement of ≤ 160 eV@4 keV. Additionally, the time resolution is ∼ 4 μ s , complying with the design requirement of ≤ 10 μ s . The calibration database now includes the ground calibration results of CATCH -1, establishing a dependable basis for future data analysis. The development experience, calibration, and test results of this detector system will also provide a solid foundation for subsequent tasks such as CATCH -2.
AbstractList CATCH-1, as the first satellite of Chasing All Transients Constellation Hunters (CATCH) space mission, was successfully launched into its expected orbit on June 22, 2024. The flight model underwent environmental tests before launch, including thermal cycling, thermal vacuum, and mechanical evaluations. The CATCH-1 detector system is equipped with a 4-pixel Silicon Drift Detector (SDD) array. To ensure the reliability and redundancy of the CATCH-1 detector system, two sets of data acquisition systems were independently designed and calibrated. Our focus is on presenting the ground calibration results of CATCH-1, which demonstrate a strong linear correlation between energy and channel. The main data acquisition system achieves an energy resolution of ∼ 120 eV@4 keV, while the backup data acquisition system has a slightly lower energy resolution of around 150 eV@4 keV, both meeting the design requirement of ≤ 160 eV@4 keV. Additionally, the time resolution is ∼4μs, complying with the design requirement of ≤10μs. The calibration database now includes the ground calibration results of CATCH-1, establishing a dependable basis for future data analysis. The development experience, calibration, and test results of this detector system will also provide a solid foundation for subsequent tasks such as CATCH-2.
CATCH -1, as the first satellite of Chasing All Transients Constellation Hunters ( CATCH ) space mission, was successfully launched into its expected orbit on June 22, 2024. The flight model underwent environmental tests before launch, including thermal cycling, thermal vacuum, and mechanical evaluations. The CATCH -1 detector system is equipped with a 4-pixel Silicon Drift Detector (SDD) array. To ensure the reliability and redundancy of the CATCH -1 detector system, two sets of data acquisition systems were independently designed and calibrated. Our focus is on presenting the ground calibration results of CATCH -1, which demonstrate a strong linear correlation between energy and channel. The main data acquisition system achieves an energy resolution of ∼ 120 eV@4 keV, while the backup data acquisition system has a slightly lower energy resolution of around 150 eV@4 keV, both meeting the design requirement of ≤ 160 eV@4 keV. Additionally, the time resolution is ∼ 4 μ s , complying with the design requirement of ≤ 10 μ s . The calibration database now includes the ground calibration results of CATCH -1, establishing a dependable basis for future data analysis. The development experience, calibration, and test results of this detector system will also provide a solid foundation for subsequent tasks such as CATCH -2.
ArticleNumber 5
Author Cao, Jiewei
Zhou, Heng
Zhao, Zijian
Zhang, Shuang-Nan
Yang, Sheng
Zhang, Yifan
Yang, Shuai
Li, Panping
Tao, Lian
Yin, Qian-Qing
Huang, Yiming
Sun, Liang
Hou, Shu-Jin
Ma, Xiang
Li, Zhengwei
Ma, Ruican
Wang, Jinzhou
Zhao, Kang
Yang, Yong
Huang, Guoli
Xiong, Shaolin
Song, Liming
Huang, Yue
He, Huilin
Li, YaJun
Wang, Yusa
Zhao, Qingchang
Wen, Xiangyang
Chen, Wen
Meng, Bin
Gao, Min
Zhao, Shujie
Xiao, Jingyu
Liu, Xiaojing
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Snippet CATCH -1, as the first satellite of Chasing All Transients Constellation Hunters ( CATCH ) space mission, was successfully launched into its expected orbit on...
CATCH-1, as the first satellite of Chasing All Transients Constellation Hunters (CATCH) space mission, was successfully launched into its expected orbit on...
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SubjectTerms Astronomy
Calibration
Chemistry and Earth Sciences
Computer Science
Data acquisition
Data acquisition systems
Data analysis
Energy resolution
Environmental testing
Flight
Focal plane
Ground tests
Observations and Techniques
Physics
Physics and Astronomy
Redundancy
Satellite constellations
Sensors
Space missions
Statistics for Engineering
System reliability
Thermal cycling
Title Ground testing and calibration of focal plane detector flight model on board the first pathfinder of CATCH
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