Ion Velocity Characterization of the 12.5-kW Advanced Electric Propulsion System Engineering Hall Thruster-Reference-Cited by-同舟云学术

Ion Velocity Characterization of the 12.5-kW Advanced Electric Propulsion System Engineering Hall Thruster

Published:2021-07-28 Issue: Volume: Page:
ISSN:
Container-title:AIAA Propulsion and Energy 2021 Forum
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Author:

Huang Wensheng¹,Frieman Jason D.¹,Kamhawi Hani¹,Peterson Peter Y.¹,Hofer Richard R.²,Branch Nicholas A.³,Dao Hoang³

Affiliation:

1. NASA Glenn Research Center

2. Jet Propulsion Laboratory, California Institute of Technology

3. Aerojet Rocketdyne

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3432

Reference29 articles.

1. SpaceNews. NASA refines plans for launching Gateway and other Artemis elements. 2020 May 14 [cited; Available from: https://spacenews.com/nasa-refines-plans-for-launching-gateway-and-other-artemis-elements/.

2. NASA. NASA Awards Artemis Contract for Lunar Gateway Power, Propulsion. 2019 [cited; Available from: https://www.nasa.gov/press-release/nasa-awards-artemis-contract-for-lunar-gateway-power-propulsion.

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

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3. The Dispersion of Lower-Hybrid Instabilities and Comparisons with Measurements Near the Front Pole of a Magnetically Shielded Hall Thruster;AIAA SCITECH 2023 Forum;2023-01-19

4. Plasma structure and electron cross-field transport induced by azimuthal manipulation of the radial magnetic field in a Hall thruster E × B discharge;Journal of Applied Physics;2022-02-07