Electrospray Propulsion

Electrospray Propulsion is a type of electric propulsion that generates thrust by emitting charged droplets or ions from a liquid propellant under a strong electric field, distinguishing it through the use of field-induced emission mechanisms for propellant acceleration.

127

Publications

4.3K

Citations

300

Authors

104

Institutions

Publications per year

2017–2026

60

Authors

300

  1. PL
    Paulo Lozano

    Massachusetts Institute of Technology, United States

    16 publications · 654 citations

    13

    h-index

  2. RE
    Richard E. Wirz

    University of California, Los Angeles, United States

    11 publications · 361 citations

    11

    h-index

  3. JS
    John Stark

    Queen Mary University of London, United Kingdom

    9 publications · 289 citations

    9

    h-index

  4. DG
    Daniel G. Courtney

    École Polytechnique Fédérale de Lausanne, Switzerland

    8 publications · 291 citations

    8

    h-index

  5. JL
    Joshua L. Rovey

    Missouri University of Science and Technology, United States

    8 publications · 314 citations

    8

    h-index

1–5 of 300

Venues

  1. Journal of Propulsion and Power

    16 publications · 918 citations

    14

    h-index

  2. Journal of Aerosol Science

    9 publications · 399 citations

    9

    h-index

  3. Journal of Applied Physics

    9 publications · 255 citations

    9

    h-index

  4. Aerospace

    5 publications · 192 citations

    5

    h-index

  5. Journal of Spacecraft and Rockets

    4 publications · 255 citations

    4

    h-index

1–5