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Cited by 50Spacecraft and Cryogenic TechnologiesHeat transfer and supercritical fluidsRocket and propulsion systems research

Analysis of Thermal Stratification of Liquid Hydrogen in Rocket Propellant Tanks

Tatom, J. W., Brown, W. H., Knight, L. H., Coxe, E. F.·1964·Advances in Cryogenic Engineering
DOI 10.1007/978-1-4757-0525-6_31
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Crossref · 10.1007/978-1-4757-0525-6_31

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  • If the warmer stratified layers enter the rocket propellant feed system, pump cavitation can occur, which could potentially destroy the rocket.

    “If the warmer stratified layers enter the rocket propellant feed system, pump cavitation can occur, which could potentially destroy the rocket [35].”

    From Modelling of Liquid Hydrogen Boil-Off (2022) · cites this paper as [35]

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  • Modelling of Liquid Hydrogen Boil-Off

    Al Ghafri, S. Z. S., Swanger, A., Jusko, V., Siahvashi, A., Perez, F., Johns, M. L., & May, E. F. (2022) · Energies · doi:10.3390/en15031149 · Cited by 131 · see citing works

    “If the warmer stratified layers enter the rocket propellant feed system, pump cavitation can occur, which could potentially destroy the rocket [35].”
    Background

Authors
Tatom, J. W., Brown, W. H., Knight, L. H., & Coxe, E. F.
Venue
Advances in Cryogenic Engineering
Publisher
Springer US
Published
1964
Pages
265-272
DOI
10.1007/978-1-4757-0525-6_31
OpenAlex
W16451293
Cited by
50
References
0
Citations by year
2026: 3 · 2025: 3 · 2024: 2 · 2023: 3 · 2022: 2 · 2021: 3 · 2020: 1 · 2019: 2 · 2018: 3 · 2017: 3 · 2016: 1 · 2015: 1 · 2013: 3
FWCI
8.07
Type
book chapter
Language
en
Open access
closed
Locations
Springer eBooks (publishedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft and Cryogenic Technologies
  • Physical Sciences › Engineering › Computational Mechanics › Heat transfer and supercritical fluids
  • Physical Sciences › Engineering › Aerospace Engineering › Rocket and propulsion systems research
Keywords
liquid hydrogen, thermal stratification, liquid-vapor interface, pump cavitation, propellant utilization, cryogenic propellants

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