Liquid Rocket Engines

Liquid Rocket Engines is a chemical rocket propulsion system that generates thrust by burning liquid propellants—stored in separate tanks and delivered under pressure to a combustion chamber—so that the high-temperature, high-velocity exhaust gases produced are expanded and expelled through a nozzle.

484

Publications

16.1K

Citations

1.1K

Authors

279

Institutions

Publications per year

2017–2026

119

Authors

1.1K

  1. FN
    Francesco Nasuti

    Sapienza University of Rome, Italy

    12 publications · 330 citations

    11

    h-index

  2. JK
    Jaye Koo

    Korea Aerospace University, South Korea

    10 publications · 244 citations

    10

    h-index

  3. MS
    Min Son

    Korea Aerospace University, South Korea

    9 publications · 230 citations

    9

    h-index

  4. YY
    Youngbin Yoon

    Seoul National University, South Korea

    8 publications · 202 citations

    8

    h-index

  5. BC
    Bruce Chehroudi

    Edwards Air Force Base, United States

    8 publications · 726 citations

    8

    h-index

1–5 of 1.1K

Venues

  1. Journal of Propulsion and Power

    62 publications · 3.3K citations

    32

    h-index

  2. Acta Astronautica

    25 publications · 1K citations

    20

    h-index

  3. NASA Technical Reports Server (NASA)

    Repository · 15 publications · 889 citations

    13

    h-index

  4. Aerospace Science and Technology

    AST · 12 publications · 386 citations

    12

    h-index

  5. Aerospace

    8 publications · 150 citations

    10

    h-index

1–5