Ablative Cooling

Ablative Cooling is a thermal protection method in which a material absorbs and dissipates heat through controlled decomposition and mass loss, thereby shielding rocket propulsion systems from extreme temperatures.

34

Publications

1.3K

Citations

138

Authors

54

Institutions

Publications per year

2017–2026

8

Authors

138

  1. HE
    H. E. Goldstein

    Ames Research Center, United States

    2 publications · 89 citations

    2

    h-index

  2. ZZ
    Zhihua Zhou

    Tianjin University, China

    2 publications · 108 citations

    2

    h-index

  3. JH
    Jürgen Heinemann

    Ames Research Center, United States

    2 publications · 89 citations

    2

    h-index

  4. IT
    Imelda Terrazas-Salinas

    Ames Research Center, United States

    2 publications · 89 citations

    2

    h-index

  5. JL
    Junwei Liu

    Tianjin University, China

    2 publications · 108 citations

    2

    h-index

1–5 of 138

Venues

  1. Journal of Spacecraft and Rockets

    4 publications · 146 citations

    4

    h-index

  2. Fusion Engineering and Design

    3 publications · 68 citations

    3

    h-index

  3. AIAA Journal

    2 publications · 94 citations

    2

    h-index

  4. Solar Energy Materials and Solar Cells

    2 publications · 126 citations

    2

    h-index

  5. 1

    h-index

1–5