Rocket Combustion

Rocket Combustion is a high-energy exothermic chemical reaction process within the broader domain of propulsion systems, specifically distinguished by the controlled burning of fuel and oxidizer in liquid rocket engines to generate high-pressure and high-temperature gases that produce thrust through expansion in a nozzle.

1.1K

Publications

39.1K

Citations

2.6K

Authors

602

Institutions

Publications per year

2017–2026

291

Authors

2.6K

  1. MO
    Michael Oschwald

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    21 publications · 675 citations

    15

    h-index

  2. OH
    Oskar Haidn

    Technical University of Munich, Germany

    23 publications · 598 citations

    15

    h-index

  3. GA
    Grant A. Risha

    Pennsylvania State University, United States

    15 publications · 553 citations

    13

    h-index

  4. SF
    Steven F. Son

    Purdue University West Lafayette, United States

    11 publications · 269 citations

    12

    h-index

  5. WM
    W. Mayer

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    12 publications · 853 citations

    12

    h-index

1–5 of 2.6K

Venues

  1. Journal of Propulsion and Power

    124 publications · 6K citations

    44

    h-index

  2. Acta Astronautica

    48 publications · 1.8K citations

    26

    h-index

  3. AIAA Journal

    51 publications · 1.7K citations

    25

    h-index

  4. Aerospace Science and Technology

    AST · 29 publications · 1.2K citations

    23

    h-index

  5. Combustion and Flame

    34 publications · 1.7K citations

    21

    h-index

1–5