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A Combustion Test Program to Establish Design Criteria for Liquid-Hydrogen-Fueled Space Vehicles

  • S. W. Wolfe
  • R. F. Yurczyk
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 10)

Abstract

Recent development of liquid hydrogen as a fuel for space vehicles has created a requirement to establish design criteria which will eliminate potential hazards due to propellant leakage or venting into confined areas.

Keywords

Peak Pressure Initial Pressure Pressure Rise Cryogenic Temperature Space Vehicle 
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.
    I. L. Drell and F. E. Belles, “Survey of Hydrogen Combustion Properties,” NACA Report 1383.Google Scholar
  2. 2.
    B. Lewis and G. Von Elbe, Combustion, Flames, and Explosions of Gases, Academic Press (1961).Google Scholar

Copyright information

© Plenum Press, New York 1965

Authors and Affiliations

  • S. W. Wolfe
    • 1
  • R. F. Yurczyk
    • 1
  1. 1.General Dynamics/AstronauticsSan DiegoUSA

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