Experimental Performance and Selection of Cryogenic Rocket Insulation Systems

  • R. J. Frainier
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 6)

Abstract

There appears to be general agreement that the next generation of rockets developed for both manned and unmanned exploration of space will utilize liquid O2-H2 propellant systems. Hydrogen also appears as an attractive working fluid for the nuclear and ion engines now in the research stage.

Keywords

Liquid Hydrogen Staging Time Insulation System Model Tank 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.
    C.M. Schmidt and A. J. Honowalt, “Skin Temperatures of a Satellite,” jet Propulsion, Vol. 27, No. 10 (October, 1957).Google Scholar

Copyright information

© Springer Science+Business Media New York 1961

Authors and Affiliations

  • R. J. Frainier
    • 1
  1. 1.Linde CompanyDivision of Union Carbide CorporationTonawandaUSA

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