Thrust performance, propellant ionization, and thruster erosion of an external discharge plasma thruster-Reference-Cited by-同舟云学术

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Thrust performance, propellant ionization, and thruster erosion of an external discharge plasma thruster

Published:2018-04-21 Issue:15 Volume:123 Page:153302
ISSN:0021-8979
Container-title:Journal of Applied Physics
language:en
Short-container-title:Journal of Applied Physics

Author:

Karadag Burak¹²^ORCID,Cho Shinatora³,Funaki Ikkoh¹²

Affiliation:

1. Department of Space and Astronautical Science, The Graduate University for Advanced Studies, Sagamihara, Kanagawa 252-5210, Japan

2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252-5210, Japan

3. Institute of Aeronautical Technology, Japan Aerospace Exploration Agency, Chofu, Tokyo 182-0012, Japan

Funder

Japan Aerospace Exploration Agency

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5023829

Reference35 articles.

1. Wall material effects in stationary plasma thrusters. I. Parametric studies of an SPT-100

2. Magnetic shielding of walls from the unmagnetized ion beam in a Hall thruster

3. A low-power, linear-geometry Hall plasma source with an open electron-drift

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