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Experimental Evaluation of the Equations and Parameters Governing Flow through Multilayer Insulations during Evacuation

  • R. M. Coston
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 11)

Abstract

The majority of the cryogenic propellant storage schemes associated with long term storage aboard space vehicles incorporate multilayer insulation systems. In order to predict propellant losses during vehicle ascent and to determine the proper vent path spacing which will allow rapid depressurization of the insulation while maintaining the physical integrity of the insulation system, it is necessary to have a complete description of the flow phenomena within the insulation.

Keywords

Layer Density Radiation Shield Insulation System Pressure Decay Free Molecular Regime 
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.
    “Liquid Propeilant Losses during Space Flight,” Final Report, Contract No. NASw-615, Report No. 65008–00–04, Arthur D. Little, Inc., Cambridge, Mass. Prepared for NASA LERC, Cleveland, Ohio.Google Scholar
  2. 2.
    T. C. Nast and R. M. Coston, “Investigation of the Gas Flow within Multilayer Insulations and Its Effect on Cryogenic Space Vehicle Design,” presented at Symposium on Cryogenic Engineering in the Aerospace Industry, Fifty-Sixth National Meeting AIChE, San Francisco, California (May 1965).Google Scholar

Copyright information

© Springer Science+Business Media New York 1966

Authors and Affiliations

  • R. M. Coston
    • 1
  1. 1.Lockheed Missiles and Space CompanyPalo AltoUSA

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