The far-field plasma characteristics of LHT40 low-power Hall thruster for commercial aerospace applications-Reference-Cited by-同舟云学术

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The far-field plasma characteristics of LHT40 low-power Hall thruster for commercial aerospace applications

Published:2021-09-14 Issue:10 Volume:23 Page:104009
ISSN:1009-0630
Container-title:Plasma Science and Technology
language:
Short-container-title:Plasma Sci. Technol.

Author:

CHEN Xinwei,GU Zuo,GAO Jun,WANG Shangmin,CHEN Tao,GUO Ning,YANG Sanxiang,LIU Chao

Funder

Military Test Instruments Program

Key Laboratory Funds for Science and Technology on Vacuum Technology and Physics Laboratory

National Natural Science Foundation of China

Science and Technology Plan of Gansu Province

Publisher

IOP Publishing

Subject

Condensed Matter Physics

Link

https://iopscience.iop.org/article/10.1088/2058-6272/ac15eb/pdf

Reference33 articles.

1. Electric propulsion for satellites and spacecraft: established technologies and novel approaches

2. Parametric investigations of a nonconventional Hall thruster

3. Fundamentals of stationary plasma thruster theory;Morozov,2000

4. Two years of on-orbit performance of SPT-100 electric propulsion;Pidgeon,2006

5. Demonstration of 10,400 h of operation on 4.5 kW qualification model hall thruster;De Grys,2017

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Perturbation indicator for Hall effect thruster operating state based on statistical characteristics of breathing oscillation time scale signals;Advances in Space Research;2023-11

2. Analysis and Experimental Validation of an Integrated Current-Source Power Supply With High Power Factor for DBD Applications;IEEE Transactions on Plasma Science;2023-05

3. Study of beam divergence and thrust vector eccentricity characteristics of the Hall thruster based on dual Faraday probe array planes and its applications;Plasma Science and Technology;2023-02-21

4. Numerical study of the effect of aft-loaded magnetic field on multiple ionizations in Hall thruster;Plasma Science and Technology;2022-06-08

5. Experimental and numerical simulation study of the effect for the anode positions on the discharge characteristics of 300 W class low power Hall thrusters;Plasma Science and Technology;2022-01-01

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