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

Authors

1.3K

  1. RR
    Richard R. Hofer

    Jet Propulsion Laboratory, United States

    85 publications · 4.2K citations

    42

    h-index

  2. YR
    Yevgeny Raitses

    Princeton Plasma Physics Laboratory, United States

    73 publications · 3.9K citations

    39

    h-index

  3. NJ
    N. J. Fisch

    Princeton University, United States

    52 publications · 3K citations

    33

    h-index

  4. IG
    Ioannis G. Mikellides

    Jet Propulsion Laboratory, United States

    49 publications · 2.5K citations

    30

    h-index

  5. DM
    Dan M. Goebel

    Jet Propulsion Laboratory, United States

    47 publications · 2.4K citations

    28

    h-index

1–5 of 1.3K

Venues

  1. Physics of Plasmas

    143 publications · 8.2K citations

    52

    h-index

  2. Journal of Propulsion and Power

    102 publications · 4.4K citations

    41

    h-index

  3. Journal of Applied Physics

    67 publications · 3.8K citations

    35

    h-index

  4. IEEE Transactions on Plasma Science

    51 publications · 1.7K citations

    28

    h-index

  5. Plasma Sources Science and Technology

    59 publications · 2.1K citations

    28

    h-index

1–5