Thrust Chamber Design

Thrust Chamber Design is a methodological framework within the field of rocket propulsion that specifies the systematic integration of geometric, thermodynamic, and material parameters to optimize combustion efficiency, heat transfer management, and structural integrity in the combustion chamber and nozzle assembly of liquid rocket engines.

106

Publications

2.7K

Citations

314

Authors

93

Institutions

Publications per year

2017–2026

12

Authors

314

  1. OK
    O. Knab

    Airbus (Germany), Germany

    5 publications · 125 citations

    5

    h-index

  2. JK
    Joachim Kretschmer

    Daimler (Germany), Germany

    4 publications · 58 citations

    4

    h-index

  3. AH
    Armin Herbertz

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

    4 publications · 77 citations

    4

    h-index

  4. BS
    Bing Sun

    Beihang University, China

    3 publications · 63 citations

    3

    h-index

  5. OH
    Oskar Haidn

    Technical University of Munich, Germany

    3 publications · 68 citations

    3

    h-index

1–5 of 314

Venues

  1. Journal of Spacecraft and Rockets

    19 publications · 374 citations

    13

    h-index

  2. Acta Astronautica

    8 publications · 258 citations

    7

    h-index

  3. Vacuum

    5 publications · 172 citations

    5

    h-index

  4. Aerospace Science and Technology

    AST · 3 publications · 78 citations

    3

    h-index

  5. Journal of Propulsion and Power

    3 publications · 137 citations

    3

    h-index

1–5