Measurement and diagnosis of miniaturized ion thruster plume

Author:

Yang Yunfan1ORCID,Zhou Siyin1ORCID,Yan Kang1,Wang Zitong1,Zhang Zun2,Nie Wansheng1

Affiliation:

1. Department of Aerospace Science and Technology, Space Engineering University 1 , Beijing 101416, People’s Republic of China

2. School of Space and Environment, Beihang University 2 , Beijing 100191, People’s Republic of China

Abstract

A planar Langmuir probe, which can be used for both ion electric propulsion beam characteristics measurement and plasma diagnosis, was developed and applied to plume measurement and diagnosis experiments of an 8 cm Kaufman ion thruster to address the growing demand for miniaturized ion thruster plume measurement and diagnosis. The experimental results show that the plume area exhibits good symmetry along the central axis, and the beam dispersion angle of the 8 cm ion thruster is approximately 22.7°. The radial distributions of the floating potential, plasma space potential and ion density are similar, showing a high distribution in the middle and a relatively low distribution at the two ends. The miniaturized ion thruster plume measurement and diagnosis system is not only easy to manipulate, but also fast and efficient for plasma plume measurement and diagnosis, which provides more complete data support for analyzing the working state of the miniaturized ion thrusters and optimizing the design of the thruster structure.

Funder

National Natural Science Foundation of China

Natural Science Foundation of Beijing Municipality

Publisher

AIP Publishing

Subject

General Physics and Astronomy

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