Cryopumping Rocket Exhaust Products at High Throughputs and Low Pressure

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

Abstract

Preliminary analyses for the design of a cryopumping system to freeze out large-mass flow rates of rocket exhaust products are presented in this report. The controlling design factors, results of preliminary analysis, and test data to show feasibility, are included.

Keywords

Heat Exchanger Knudsen Number Space Simulation Plate Spacing Exhaust Product 
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.
    B.M. Bailey and R.L. Chuan, “Gryopuinpingfor High Vacuum with Low Power,” Fifth. National Symposium on Vacuum Technology Transactions, American Vacuum Society, Pergaraon Press, New York (1958), p. 262.Google Scholar

Copyright information

© Springer Science+Business Media New York 1962

Authors and Affiliations

  • R. O. Barkdoll
    • 1
  • J. W. Anderson
    • 1
  1. 1.General Dynamics/ConvairSan DiegoUSA

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