Hall Effect Thrusters
Hall Effect Thrusters is an electric propulsion device that generates thrust by accelerating ionized propellant through an electrostatic field established in a plasma channel, where electrons are confined by a radial magnetic field to enhance ionization efficiency and enable high-specific-impulse performance.
981
Publications
35.8K
Citations
1.3K
Authors
326
Institutions
Publications per year
2017–2026
228
981
Plasma oscillations in Hall thrusters
Edgar Choueiri · Physics of Plasmas · 2001 · 510 citations
Tutorial: Physics and modeling of Hall thrusters
Jean-Pierre Bœuf · Journal of Applied Physics · 2017 · 463 citations
Plasmas for spacecraft propulsion
Christine Charles · Journal of Physics D Applied Physics · 2009 · 356 citations
Parametric investigations of a nonconventional Hall thruster
Yevgeny Raitses, N. J. Fisch · Physics of Plasmas · 2001 · 207 citations
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326
University of Michigan
Ann Arbor, United States
46 h-index
264 publications
10.9K citations
Jet Propulsion Laboratory
Pasadena, United States
40 h-index
270 publications
12.8K citations

Princeton Plasma Physics Laboratory
Princeton, United States
40 h-index
210 publications
11.7K citations

Centre National de la Recherche Scientifique
Paris, France
37 h-index
278 publications
13.3K citations

Glenn Research Center
Cleveland, United States
31 h-index
208 publications
6K citations
Princeton University
Princeton, United States
30 h-index
139 publications
7.8K citations
Institut de Combustion Aérothermique Réactivité et Environnement
Orléans, France
28 h-index
89 publications
3.9K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
24 h-index
63 publications
2.6K citations
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143 publications · 8.2K citations
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102 publications · 4.4K citations
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67 publications · 3.8K citations
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59 publications · 2.1K citations
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