Cited by 23Spacecraft and Cryogenic TechnologiesHydrogen Storage and MaterialsHeat transfer and supercritical fluids

Hydrogen No-Vent Fill Testing in a 34 Liter (1.2 Cubic Foot) Tank

Moran, Matthew E., Nyland, Ted W., Driscoll, Susan L.·1992·Advances in Cryogenic Engineering

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Crossref · 10.1007/978-1-4615-3368-9_59

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  • Many studies have investigated how to minimize boil-off losses and empirically determined that top fill (spray) is the most effective way to reduce transfer losses during loading, but the underlying physics remains poorly understood.

    “While many studies [71][72][73][74][75][76][77][78][79][80][81][82][83][84] have investigated how to minimize boil-off losses and empirically determined that top fill (spray) is the most effective way to reduce transfer losses during loading, the underlying physics remains poorly understood.”

    From Modelling of Liquid Hydrogen Boil-Off (2022) · cites this paper as [72]

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Authors
Moran, M. E., Nyland, T. W., & Driscoll, S. L.
Affiliations
  • Glenn Research Center (US)
  • Marshall Space Flight Center (US)
Venue
Advances in Cryogenic Engineering
Publisher
Springer US
Published
1992
Pages
1257-1264
OpenAlex
W1607959056
Cited by
23
References
0
Citations by year
2026: 3 · 2025: 2 · 2024: 1 · 2023: 1 · 2022: 3 · 2021: 1 · 2020: 2 · 2015: 2 · 2012: 1
FWCI
6.73
Type
book chapter
Language
en
Open access
closed
Locations
Springer eBooks (publishedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft and Cryogenic Technologies
  • Physical Sciences › Materials Science › Materials Chemistry › Hydrogen Storage and Materials
  • Physical Sciences › Engineering › Computational Mechanics › Heat transfer and supercritical fluids
Keywords
liquid hydrogen, fill level

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