Cited by 36Spacecraft and Cryogenic TechnologiesHeat transfer and supercritical fluidsRocket and propulsion systems research

Analytical and Experimental Determination of Liquid-Hydrogen Temperature Stratification

Bailey, T. E., Fearn, R. F.·1964·Advances in Cryogenic Engineering

Integrity signals

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Crossref · 10.1007/978-1-4757-0525-6_30

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  • Currently, the space industry is an important user of LH2, with long duration storage of cryogenic hydrogen being essential in orbital transfer vehicles, the upper stages of rockets, and deep space exploration probes.

    “Currently, the space industry is an important user of LH 2 , with long duration storage of cryogenic hydrogen being essential in orbital transfer vehicles, the upper stages of rockets, and deep space exploration probes [29][30][31][32][33][34].”

    From Modelling of Liquid Hydrogen Boil-Off (2022) · cites this paper as [31]

  • Boil-off is particularly important during atmospheric departure, where frictional drag forces result in substantial heat ingress into the containment vessel, thereby increasing vapor temperature and pressure.

    “Boil-off is particularly important during atmospheric departure, where frictional drag forces result in substantial heat ingress into the containment vessel, thereby increasing vapor temperature and pressure [31].”

    From Modelling of Liquid Hydrogen Boil-Off (2022) · cites this paper as [31]

Cited by

Sorted by citations

Authors
Bailey, T. E., & Fearn, R. F.
Venue
Advances in Cryogenic Engineering
Publisher
Springer US
Published
1964
Pages
254-264
OpenAlex
W1033457511
Cited by
36
References
0
Citations by year
2026: 2 · 2025: 4 · 2024: 5 · 2023: 1 · 2022: 4 · 2021: 1 · 2018: 2 · 2017: 1 · 2013: 2
FWCI
5.38
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, propellant tanks, cryogenic propellants, vapor pressure, aerodynamic heating, boost phase, net positive suction head, tank pressure, aerial vehicles

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Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.

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