title: A microNewton thrust stand for average thrust measurement of pulsed microthruster.
abstract: A torsional thrust stand has been developed for the study of the average thrust for microNewton pulsed thrusters. The main body of the thrust stand mainly consists of a torsional balance, a pair of flexural pivots, a capacitive displacement sensor, a calibration assembly, and an eddy current damper. The behavior of the stand was thoroughly studied. The principle of thrust measurement was analyzed. The average thrust is determined as a function of the average equilibrium angle displacement of the balance and the spring stiffness. The thrust stand has a load capacity up to 10 kg, and it can theoretically measure the force up to 609.6 μN with a resolution of 24.4 nN. The static calibrations were performed based on the calibration assembly composed of the multiturn coil and the permanent magnet. The calibration results demonstrated good repeatability (less than 0.68% FSO) and good linearity (less than 0.88% FSO). The assembly of the multiturn coil and the permanent magnet was also used as an exciter to simulate the microthruster to further research the performance of the thrust stand. Three sets of force pulses at 17, 33.5, and 55 Hz with the same amplitude and pulse width were tested. The repeatability error at each frequency was 7.04%, 1.78%, and 5.08%, respectively.
authors.affiliation: State Key Laboratory of Laser Propulsion & Application, Academy of Equipment, Beijing 101416, China.
authors.forename: Wei-Jing
authors.initials: WJ
authors.lastname: Zhou
authors.affiliation: State Key Laboratory of Laser Propulsion & Application, Academy of Equipment, Beijing 101416, China.
authors.forename: Yan-Ji
authors.initials: YJ
authors.lastname: Hong
authors.affiliation: State Key Laboratory of Laser Propulsion & Application, Academy of Equipment, Beijing 101416, China.
authors.forename: Hao
authors.initials: H
authors.lastname: Chang