Radial position effects of externally mounted hollow cathode on a magnetically shielded Hall thruster

Author:

Zhong Chao1,Li Hong12ORCID,Hu Yanlin3,Wang Zhaoyu1,Ding Yongjie12ORCID,Wei Liqiu12ORCID,Yu Daren12

Affiliation:

1. Lab of Plasma Propulsion, Harbin Institute of Technology, Harbin 150001, People's Republic of China

2. Key Laboratory of Aerospace Plasma Propulsion, Ministry of Industry and Information Technology, Harbin 150001, People's Republic of China

3. Beijing Institute of Control Engineering, Beijing 100190, People's Republic of China

Abstract

A magnetically shielded Hall thruster (MSHT) has a significantly longer service life than a conventional unshielded Hall thruster (USHT) as it shifts the magnetic field of maximum strength from the channel interior to the exterior. In this study, it was experimentally determined that the influence of the radial position of an externally mounted hollow cathode on the performance of an MSHT is quite different from that of a USHT. The measured plasma parameters demonstrate that in addition to the coupling voltage loss and plume divergence loss, the electron cross-field transport loss (not considered previously and introduced by the outward shifting of the magnetic field) is also important to explaining the performance variation in the MSHT. This study refines the coupling theory between the cathode and Hall thruster and provides a valuable reference for determining the radial position of an externally mounted hollow cathode in an MSHT.

Funder

National Natural Science Foundation of China

Publisher

AIP Publishing

Subject

Physics and Astronomy (miscellaneous)

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