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Hu  RenXiang  Shan  Xu  Yuan  GuangYuan  Wang  ShuWen  Zhang  WeiHang  Qi  Wei  Cao  Zhe  Li  YiRen  Chen  ManMing  Yang  XiaoPing  Wang  Bo  Shao  SiPei  Li  Feng  Zhong  XiaoQing  Fan  Dan  Hao  XinJun  Feng  ChangQing  Su  ZhenPeng  Shen  ChengLong  Li  Xin  Dai  GuYue  Qiu  BingLin  Pan  ZongHao  Liu  Kai  Xu  ChunKai  Liu  ShuBin  An  Qi  Zhang  TieLong  Wang  YuMing 《中国科学:技术科学(英文版)》2019,62(6):1015-1027
A low-energy ion spectrometer(LEIS) for use aboard three-axis stabilized spacecraft has been developed to measure ion energy per charge distribution in three-dimensional space with good energy-, angular-and temporal-resolutions. For the standard top-hat electrostatic analyzer used widely in space plasma detection, three-axis stabilized spacecraft makes it difficult to obtain complete coverage of all possible ion arrival directions. We have designed angular scanning deflectors supplementing to a cylindrically symmetric top-hat electrostatic analyzer to provide a half-space field of view as 360°×90°(–45°–+45°), and fabricated the LEIS flight model for detecting magnetospheric ions in geosynchronous orbit. The performance of this payload has been evaluated in detail by a series of simulation and environmental tests, and the payload has also been calibrated through laboratory experiments using a low-energy ion source. The results show that capabilities of the LEIS payload are in accordance with the requirements of a magnetospheric mission.  相似文献   
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