Turbopump Design

Turbopump Design is a specialized engineering methodology within rocket propulsion systems that entails the systematic development and integration of high-speed pump and turbine components to achieve efficient, reliable delivery of propellants to the combustion chamber under extreme operational conditions.

116

Publications

2.9K

Citations

316

Authors

102

Institutions

Publications per year

2017–2026

15

Authors

316

  1. KK
    Kenjiro Kamijo

    Tohoku University, Japan

    7 publications · 342 citations

    7

    h-index

  2. JK
    Jin-Han Kim

    Korea Aerospace Research Institute, South Korea

    5 publications · 94 citations

    5

    h-index

  3. CC
    Chang‐Ho Choi

    Pohang Iron and Steel (South Korea), South Korea

    4 publications · 73 citations

    4

    h-index

  4. DW
    D. W. Childs

    Texas A&M University, United States

    4 publications · 153 citations

    4

    h-index

  5. ML
    Meng‐Sing Liou

    Glenn Research Center, United States

    3 publications · 193 citations

    3

    h-index

1–5 of 316

Venues

  1. Vacuum

    9 publications · 196 citations

    9

    h-index

  2. Journal of Propulsion and Power

    8 publications · 352 citations

    8

    h-index

  3. 7

    h-index

  4. Journal of Fluids Engineering

    5 publications · 195 citations

    5

    h-index

  5. Aerospace Science and Technology

    AST · 4 publications · 76 citations

    4

    h-index

1–5