Effect of Convection in Helium-Charged, Partial-Foam Insulations for Liquid Hydrogen Propellant Tanks

  • B. N. Taylor
  • F. E. Mack
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 11)

Abstract

Liquid hydrogen, because of its low density and extremely low boiling point, requires very effective insulation during its storage and use as a fuel for space booster applications. For space booster. insulation is required to prevent excessive boiloff during the prelaunch phase and to minimize stratification during the boost phase. Minimizing stratification is essential in meeting the NPSH requirements of the rocket engines’ turbine pumps.

Keywords

Rayleigh Number Free Convection Honeycomb Core Total Heat Flow Core Thickness 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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    J. F. Haskins and J. Hertz, in: Advances in Cryogenic Engineering, Vol 7, Plenum Press, New York (1962), p. 353.Google Scholar

Copyright information

© Springer Science+Business Media New York 1966

Authors and Affiliations

  • B. N. Taylor
    • 1
  • F. E. Mack
    • 1
  1. 1.North American Aviation, Inc.DowneyUSA

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