Research Progress of Micro Thrust Measurement Technology for Space Electrical Propulsion

被引：0
|
作者：
Tang H.-B. [1 ,2 ,3 ]
Zhang Z.-K. [4 ]
Zhang Z. [4 ]
机构：
[1] School of Astronautics, Beihang University, Beijing
[2] Key Laboratory of Space Environment Monitoring and Information Processing, Ministry of Industry and Information Technology, Beijing
[3] Key Laboratory of Spacecraft Design Optimization & Dynamic Simulation Technologies, Ministry of Education, Beijing
[4] School of Space and Environment, Beihang University, Beijing
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2023年 / 44卷 / 06期
关键词：
Electric propulsion; Magnetic levitation thrust measurement; Micro-thrust calibration; Micro-thrust measurement; Review; Thrust pendulum;
D O I：
10.13675/j.cnki.tjjs.2301001
中图分类号：
学科分类号：
摘要：
The current researches of micro-thrust measurement technology applied to the space electrical propulsion are reviewed in this paper. The history of the widely used micro-thrust measurement methods are reviewed，and the torsional pendulum，suspending pendulum and inverted pendulum，balance，and indirect measurement devices，and magnetic levitation thrust measurement devices are introduced. The standard force calibration technology is reviewed，and the micro thrust calibration methods with force source and without force source are presented. According to the characteristics of the micro-thrust measurement device itself，the noise response of its performance evaluation method interacting with the environment is introduced. Finally，the characteristics of micro thrust measurement technology are analysed and the understanding of the continuous research and application of this technology is discussed. © 2023 Journal of Propulsion Technology. All rights reserved.
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