Design of a Compact Time-of-Flight Mass Spectrometer for Space Application
Design of a Compact Time-of-Flight Mass Spectrometer for Space Application
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空间应用紧凑型飞行时间质谱仪的设计
DOI:
10.1021/jasms.9b00092
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发表时间:
2020
影响因子:
3.2
通讯作者:
Huang Zhengxu
中科院分区:
文献类型:
--
作者:
Ren Zhengyi;Guo Meiru;Cheng Yongjun;Sun Wenjun;Li Gang;Dong Meng;Li Yali;Xi Zhenhua;Pei Xiaoqiang;Niu Hongzhi;Tan Guobin;Zhou Zhen;Huang Zhengxu
A miniature reflectron time-of-flight mass spectrometer (TOF MS) with orthogonal extraction coupled with electron impact (EI) ionization source can be used to perform in situ gas composition analysis in a planetary environment. However, performances such as the mass resolution, sensitivity, limit of detection, mass range, and mass accuracy are often decreased because of miniaturization. Herein, a compact instrument for space applications has been developed, and its performance has been evaluated. The mass of the TOF MS is 13.4 kg, with dimensions of 300 mm × 200 mm × 200 mm, and the power consumption is 25 W. In this paper, the design of the ion source, mass analyzer, and detector is discussed in detail. The upper limit of the mass range is greater than 500 amu, and the best resolving power obtained so far on the miniature TOF MS is around 405 at full width half maximum (FWHM); other performance indexes of the instrument are also determined, where the worst case for mass stability is 0.49%, together with a mass accuracy of 0.12% and a sensitivity of 0.6 mV/ppm.