Composite Nozzles

"Composite Nozzle" is a type of rocket propulsion nozzle constructed from layered or heterogeneous materials engineered to achieve enhanced thermal, mechanical, and structural performance compared to conventional metallic nozzles.

42

Publications

1.5K

Citations

161

Authors

66

Institutions

Publications per year

2017–2026

15

Variants

Composite Nozzle

Authors

161

  1. LC
    Laifei Cheng

    Northwestern Polytechnical University, China

    2 publications · 47 citations

    2

    h-index

  2. ST
    S. T. Keswani

    Pennsylvania State University, United States

    2 publications · 123 citations

    2

    h-index

  3. KK
    K. K. Kuo

    Pennsylvania State University, United States

    2 publications · 123 citations

    2

    h-index

  4. XL
    Xingang Luan

    Northwestern Polytechnical University, China

    2 publications · 47 citations

    2

    h-index

  5. LZ
    Litong Zhang

    Northwestern Polytechnical University, China

    2 publications · 47 citations

    2

    h-index

1–5 of 161

Venues

  1. Carbon

    4 publications · 266 citations

    4

    h-index

  2. Journal of Propulsion and Power

    2 publications · 168 citations

    2

    h-index

  3. Composites Part B Engineering

    2 publications · 114 citations

    2

    h-index

  4. Composite Structures

    2 publications · 29 citations

    2

    h-index

  5. 2

    h-index

1–5