Performance, Facility Pressure Effects, and Stability Characterization Tests of NASA’s 12.5-kW Hall Effect Rocket with Magnetic Shielding Thruster-Reference-Cited by-同舟云学术

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Performance, Facility Pressure Effects, and Stability Characterization Tests of NASA’s 12.5-kW Hall Effect Rocket with Magnetic Shielding Thruster

Published:2016-07-22 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Kamhawi Hani,Haag Thomas,Huang Wensheng,Yim John,Herman Daniel A.,Peterson Peter Y.,Williams George,Gilland James,Hofer Richard R.,Mikellides Ioannis G.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4826

Reference31 articles.

1. High-Power Solar Electric Propulsion for Future NASA Missions

2. Overview of the Development of the Solar Electric Propulsion Technology Demonstration Mission 12.5-kW Hall Thruster

Cited by 34 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. Temporally resolved relative krypton neutral density during breathing mode of a hall effect thruster recorded by TALIF;Journal of Electric Propulsion;2024-05-13

2. A Facility Effect Characterization Test of the BHT-6000 Hall Thruster;AIAA SCITECH 2024 Forum;2024-01-04

3. Facility Effects on the Ion Characteristics of a 12.5-Kilowatt Hall Thruster;Journal of Propulsion and Power;2023-09

4. Reduced-order particle-in-cell simulations of a high-power magnetically shielded Hall thruster;Plasma Sources Science and Technology;2023-06-01

5. Edge Wear of the Advanced Electric Propulsion System Pole Covers;AIAA SCITECH 2023 Forum;2023-01-19

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