A compound pendulum for thrust measurement of micro-Newton thruster

Author:

Xu Hao1ORCID,Gao Yong2,Mao Qiang-Bing1,Ye Liang-Wen1,Hu Zhong-Kun1ORCID,Zhang Kai1ORCID,Song Peiyi1ORCID,Li Qing1ORCID

Affiliation:

1. MOE Key Laboratory of Fundamental Physical Quantities Measurement & Hubei Key Laboratory of Gravitation and Quantum Physics, PGMF and School of Physics, Huazhong University of Science and Technology, Wuhan 430074, People’s Republic of China

2. Beijing Institute of Control Engineering, Beijing 100190, People’s Republic of China

Abstract

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 μN, and the noise is less than 0.1 μN/[Formula: see text] 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 μN with a standard uncertainty of 0.02 μN. 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) μN/V. When changing the voltage by 50 V, the change in thrust is measured to be 0.7 μN with a standard uncertainty of 0.1 μN.

Funder

National Natural Science Foundation of China

Young Top-notch Talent Cultivation Program of Hubei Province

Publisher

AIP Publishing

Subject

Instrumentation

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