Electrothermal Propulsion

Electrothermal Propulsion is a type of electric propulsion system in which thermal energy is added to a propellant through electrical heating, thereby increasing its enthalpy and enabling acceleration through a nozzle to produce thrust.

95

Publications

4.2K

Citations

284

Authors

101

Institutions

Publications per year

2017–2026

20

Authors

284

  1. YT
    Yoshinori Takao

    Kyoto University, Japan

    6 publications · 170 citations

    6

    h-index

  2. KE
    Koji Eriguchi

    Kyoto University, Japan

    6 publications · 170 citations

    6

    h-index

  3. KO
    Kouichi Ono

    Kyoto University, Japan

    6 publications · 170 citations

    6

    h-index

  4. RB
    Rodney Burton

    University of Illinois Urbana-Champaign, United States

    4 publications · 62 citations

    4

    h-index

  5. TT
    Takeshi Takahashi

    National Institute of Information and Communications Technology, Japan

    4 publications · 100 citations

    4

    h-index

1–5 of 284

Venues

  1. Journal of Propulsion and Power

    14 publications · 429 citations

    13

    h-index

  2. IEEE Transactions on Magnetics

    5 publications · 94 citations

    5

    h-index

  3. Applied Physics Letters

    3 publications · 286 citations

    3

    h-index

  4. IEEE Transactions on Plasma Science

    3 publications · 217 citations

    3

    h-index

  5. Physics of Plasmas

    2 publications · 56 citations

    2

    h-index

1–5