Propellant Slosh

Propellant Slosh is the oscillatory motion of liquid propellant within a rocket's storage tank during flight, distinguished from other fluid dynamics phenomena by its direct influence on the vehicle's stability, control, and structural loads due to time-varying mass distribution and momentum coupling.

117

Publications

3.9K

Citations

259

Authors

103

Institutions

Publications per year

2017–2026

16

Variants

Propellant Sloshing

Authors

259

  1. RJ
    R. J. Hung

    University of Alabama in Huntsville, United States

    11 publications · 361 citations

    11

    h-index

  2. HF
    Helmut F. Bauer

    Universität der Bundeswehr München, Germany

    6 publications · 222 citations

    6

    h-index

  3. SG
    Sathya Gangadharan

    Embry–Riddle Aeronautical University, United States

    5 publications · 75 citations

    5

    h-index

  4. MR
    Mahmut Reyhanoglu

    Embry–Riddle Aeronautical University, United States

    5 publications · 180 citations

    5

    h-index

  5. JS
    James Sudermann

    Kennedy Space Center, United States

    5 publications · 75 citations

    5

    h-index

1–5 of 259

Venues

  1. NASA Technical Reports Server (NASA)

    Repository · 13 publications · 409 citations

    11

    h-index

  2. AIAA Journal

    9 publications · 411 citations

    9

    h-index

  3. Journal of Spacecraft and Rockets

    7 publications · 175 citations

    7

    h-index

  4. Journal of Guidance Control and Dynamics

    6 publications · 157 citations

    6

    h-index

  5. Acta Astronautica

    5 publications · 214 citations

    5

    h-index

1–5