Development of a 12.5kW Hall Thruster for the Advanced Electric Propulsion System-Reference-Cited by-同舟云学术

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Development of a 12.5kW Hall Thruster for the Advanced Electric Propulsion System

Published:2020-08-17 Issue: Volume: Page:
ISSN:
Container-title:AIAA Propulsion and Energy 2020 Forum
language:
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Author:

Zubair Jonathan¹

Affiliation:

1. Aerojet Rocketdyne

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. [Online]. Available: investor.maxar.com/investor-news/press-release-details/2019/Maxar-Selected-to-Build-Fly-First-Element-of- NASAs-Lunar-Gateway/default.aspx.

2. Characterization Test of the 12.5-kW Advanced Electric Propulsion System Engineering Test Unit Hall Thruster

Cited by 4 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. Review of High-Power Electrostatic and Electrothermal Electric Propulsion;Journal of Propulsion and Power;2022-11

2. Hybrid plasma simulations of a magnetically shielded Hall thruster;Journal of Applied Physics;2022-03-14

3. Experimental characterization of Hall thruster breathing mode dynamics;Journal of Applied Physics;2021-10-07

4. Background Pressure Effects on the Performance of a 20 kW Magnetically Shielded Hall Thruster Operating in Various Configurations;Aerospace;2021-03-09

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