Detonation-based Propulsion

Detonation-Based Propulsion is a propulsion system concept that utilizes detonative combustion—characterized by supersonic exothermic reaction waves driven by shock compression—as its energy release mechanism, distinguishing it from deflagration-based systems that rely on subsonic flame propagation.

70

Publications

5.2K

Citations

182

Authors

72

Institutions

Publications per year

2017–2026

23

Authors

182

  1. FF
    François Falempin

    Office National d'Études et de Recherches Aérospatiales, France

    4 publications · 104 citations

    4

    h-index

  2. KK
    K. Kailasanath

    United States Naval Research Laboratory, United States

    4 publications · 766 citations

    4

    h-index

  3. JE
    J. E. Shepherd

    California Institute of Technology, United States

    4 publications · 90 citations

    4

    h-index

  4. VS
    V. S. Ivanov

    Semenov Institute of Chemical Physics, Russia

    3 publications · 78 citations

    3

    h-index

  5. EW
    E. Wintenberger

    California Institute of Technology, United States

    3 publications · 75 citations

    3

    h-index

1–5 of 182

Venues

  1. Journal of Propulsion and Power

    12 publications · 1.2K citations

    12

    h-index

  2. AIAA Journal

    5 publications · 960 citations

    5

    h-index

  3. Acta Astronautica

    4 publications · 227 citations

    3

    h-index

  4. Physics of Fluids

    2 publications · 86 citations

    2

    h-index

  5. International Journal of Hydrogen Energy

    2 publications · 48 citations

    2

    h-index

1–5