Rocket Nozzle Inserts

Rocket Nozzle Insert is a specialized component fabricated from carbon-carbon composite materials designed to line the throat or convergence zone of a rocket nozzle, providing thermal and structural resistance against high-velocity, high-temperature exhaust flows during propulsion.

12

Publications

536

Citations

43

Authors

24

Institutions

Publications per year

2017–2026

5

Authors

43

  1. RD
    Raffaele D’Elia

    Centre National de la Recherche Scientifique, France

    1 publications · 22 citations

    1

    h-index

  2. PJ
    P. J. Wurm

    Georgia Institute of Technology, United States

    1 publications · 98 citations

    1

    h-index

  3. JA
    José A. Moríñigo

    Instituto Nacional de Técnica Aeroespacial, Spain

    1 publications · 20 citations

    1

    h-index

  4. WG
    William G. Fahrenholtz

    Missouri University of Science and Technology, United States

    1 publications · 141 citations

    1

    h-index

  5. JC
    Jian Chen

    Yancheng Institute of Technology, China

    1 publications · 29 citations

    1

    h-index

1–5 of 43

Venues

  1. Aerospace Science and Technology

    AST · 2 publications · 49 citations

    2

    h-index

  2. Acta Astronautica

    2 publications · 38 citations

    2

    h-index

  3. Journal of Propulsion and Power

    2 publications · 127 citations

    2

    h-index

  4. Journal of Materials Science

    1 publications · 98 citations

    1

    h-index

  5. Defense Technical Information Center (DTIC)

    Repository · 1 publications · 14 citations

    1

    h-index

1–5