In-orbit background simulation of a type-B CATCH satellite

The Chasing All Transients Constellation Hunters (CATCH) space mission plans to launch three types of micro-satellites (A, B, and C). The type-B CATCH satellites are dedicated to locating transients and detecting their time-dependent energy spectra. A type-B satellite is equipped with lightweight Wo...

Full description

Saved in:
Bibliographic Details
Published inExperimental astronomy Vol. 56; no. 2-3; pp. 477 - 498
Main Authors Xiao, Jingyu, Qi, Liqiang, Zhang, Shuang-Nan, Tao, Lian, Li, Zhengwei, Zhang, Juan, Wen, Xiangyang, Yin, Qian-Qing, Yang, Yanji, Bu, Qingcui, Yang, Sheng, Liu, Xiaojing, Huang, Yiming, Chen, Wen, Yang, Yong, Liu, Huaqiu, Xu, Yibo, Zhao, Shujie, Zhang, Xuan, Li, Panping, Zhao, Kang, Ma, Ruican, Zhao, Qingchang, Tang, Ruijing, Rao, Jinhui, Li, Yajun
Format Journal Article
LanguageEnglish
Published Dordrecht Springer Netherlands 01.12.2023
Springer Nature B.V
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:The Chasing All Transients Constellation Hunters (CATCH) space mission plans to launch three types of micro-satellites (A, B, and C). The type-B CATCH satellites are dedicated to locating transients and detecting their time-dependent energy spectra. A type-B satellite is equipped with lightweight Wolter-I X-ray optics and an array of position-sensitive multi-pixel Silicon Drift Detectors. To optimize the scientific payloads for operating properly in orbit and performing the observations with high sensitivities, this work performs an in-orbit background simulation of a type-B CATCH satellite using the Geant4 toolkit. It shows that the persistent background is dominated by the cosmic X-ray diffuse background and the cosmic-ray protons. The dynamic background is also estimated considering trapped charged particles in the radiation belts and low-energy charged particles near the geomagnetic equator, which is dominated by the incident electrons outside the aperture. The simulated persistent background within the focal spot is used to estimate the observation sensitivity, i.e. 4.22  ×  10 - 13  erg cm - 2  s - 1 with an exposure of 10 4  s and a Crab-like source spectrum, which can be utilized further to optimize the shielding design. The simulated in-orbit background also suggests that the magnetic diverter just underneath the optics may be unnecessary in this kind of micro-satellites, because the dynamic background induced by charged particles outside the aperture is around 3 orders of magnitude larger than that inside the aperture.
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:0922-6435
1572-9508
DOI:10.1007/s10686-023-09902-y