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Gas Requirements in Pressurized Transfer of Liquid Hydrogen

  • D. F. Gluck
  • J. F. Kline
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 7)

Abstract

In the past few years liquid hydrogen has become a very popular fuel for space missions. It is being used in such programs as Centaur and Saturn. Furthermore, hydrogen is the ideal working fluid for nuclear-powered space vehicles currently under development. In these applications, liquid-hydrogen fuel is generally transferred to the combustion chamber by a combination of pumping and pressurization. The pump forces the liquid propellant from the fuel tank to the combustion chamber; gaseous pressurant holds tank pressure sufficiently high to prevent cavitation at the pump inlet and to maintain the structural rigidity of the tank.

Keywords

Heat Transfer Liquid Hydrogen Tank Wall Cylindrical Tank Heat Leak 
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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Copyright information

© Springer Science+Business Media New York 1962

Authors and Affiliations

  • D. F. Gluck
    • 1
  • J. F. Kline
    • 1
  1. 1.Lewis Research Center National Aeronautics and Space AdministrationClevelandUSA

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