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On the Bulk Density of Boiling Liquid Oxygen

  • R. W. Arnett
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 7)

Abstract

Liquid-fueled rockets often utilize one or more cryogenic fluids as propellants. For maximum efficiency it is necessary that the mass of propellants loaded aboard the missile be known with considerable accuracy. One means of achieving this end is to know both the volume of the propellant present and its mean specific weight or, as it will be called here, its bulk density.

Keywords

Bulk Density Friction Factor Head Loss Heat Balance Equation Liquid Oxygen 
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

  1. 1.
    F. Herzberg in Advances in Cryogenic Engineering, Vol.5, K.D. Timmerhaus (ed.), Plenum Press, Inc., New York (1960), p. 526.Google Scholar
  2. 2.
    R. W. Arnett, unpublished work.Google Scholar
  3. 3.
    R. B. Scotts unpublished data.Google Scholar

Copyright information

© Springer Science+Business Media New York 1962

Authors and Affiliations

  • R. W. Arnett
    • 1
  1. 1.CEL National Bureau of StandardsBoulderUSA

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