Ion flux, energy, and charge-state measurements for the BPT-4000 Hall thruster

Author:

Pollard James1,Diamant Kevin1,Khayms Vadim2,Werthman Lance2,King David3,De Grys Kristi3

Affiliation:

1. Aerospace Corp., El Segundo, CA

2. Lockheed Martin Space Systems Co., Sunnyvale, CA

3. General Dynamics Corp., Redmond, WA

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

Cited by 16 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. Influence of Field Topology on Magnetically Shielded Hall Thruster Plume Divergence;2022 IEEE Aerospace Conference (AERO);2022-03-05

2. Development of Wien Filter for a low-power Hall Thruster Plume Characterization;AIAA Propulsion and Energy 2021 Forum;2021-07-28

3. Recommended Practice for Use of Faraday Probes in Electric Propulsion Testing;Journal of Propulsion and Power;2017-05

4. High Fidelity Numerical Simulations for the Characterization of Plasma Plume Interaction Effects on Geostationary Satellites;AIAA SPACE 2015 Conference and Exposition;2015-08-28

5. Characterization of the NASA NEXT Thruster;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

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