A compound pendulum for thrust measurement of micro-Newton thruster

被引:21
作者
Xu, Hao [1 ,2 ]
Gao, Yong [3 ]
Mao, Qiang-Bing [1 ,2 ]
Ye, Liang-Wen [1 ,2 ]
Hu, Zhong-Kun [1 ,2 ]
Zhang, Kai [1 ,2 ]
Song, Peiyi [1 ,2 ]
Li, Qing [1 ,2 ]
机构
[1] Huazhong Univ Sci & Technol, MOE Key Lab Fundamental Phys Quant Measurement, Wuhan, Peoples R China
[2] Huazhong Univ Sci & Technol, PGMF & Sch Phys, Hubei Key Lab Gravitat & Quantum Phys, Wuhan, Peoples R China
[3] Beijing Inst Control Engn, Beijing 100190, Peoples R China
基金
中国国家自然科学基金;
关键词
STAND;
D O I
10.1063/5.0090980
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
A thrust stand is developed for testing micro-Newton level thrusters on the ground. The stand is composed of a compound pendulum that is symmetrically suspended by two thin beryllium copper strips, and it is precisely calibrated by gravity. The stiffness of the stand can be adjusted in 3 orders of magnitude by a counterweight. When the stiffness is larger than 1 Nm/rad, the stand demonstrates a fast response to thrust. The measured range of the stand reaches 1000 mu N, and the noise is less than 0.1 mu N root Hz within 1 mHz-1 Hz. To calibrate the resolution of the stand, an electrostatic force is applied to the stand with an actuator. The equivalent thrust is determined to be 0.09 mu N with a standard uncertainty of 0.02 mu N. Using the stand, a micro-Newton colloid thruster is tested. The output of the colloid thruster changes with the applied voltage as 0.015(1) mu N/V. When changing the voltage by 50 V, the change in thrust is measured to be 0.7 mu N with a standard uncertainty of 0.1 mu N. Published under an exclusive license by AIP Publishing.
引用
收藏
页数:8
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