Propellant Compatibility

Propellant Compatibility is a material-interaction criterion that distinguishes the degree to which a liquid rocket propellant can coexist with engine materials and components without inducing detrimental chemical or physical degradation under operational conditions.

33

Publications

798

Citations

127

Authors

37

Institutions

Publications per year

2017–2026

9

Authors

127

  1. TO
    Thomas Owens

    University of South Carolina, United States

    3 publications · 37 citations

    2

    h-index

  2. AA
    Amir Abdelaziz

    Polytechnic School of Algiers, Algeria

    2 publications · 63 citations

    2

    h-index

  3. AK
    A. K. Sikder

    High Energy Materials Research Laboratory, India

    2 publications · 55 citations

    2

    h-index

  4. DT
    Djalal Trache

    Polytechnic School of Algiers, Algeria

    2 publications · 63 citations

    2

    h-index

  5. MJ
    Michael J. Robinson

    Cranfield University, United Kingdom

    3 publications · 37 citations

    2

    h-index

1–5 of 127

Venues

  1. Propellants Explosives Pyrotechnics

    7 publications · 180 citations

    7

    h-index

  2. Journal of Propulsion and Power

    3 publications · 39 citations

    3

    h-index

  3. Defence Science Journal

    1 publications · 21 citations

    1

    h-index

  4. Combustion Explosion and Shock Waves

    1 publications · 24 citations

    1

    h-index

  5. Journal of Thermal Analysis and Calorimetry

    1 publications · 79 citations

    1

    h-index

1–5