Hydrogen Liquid Level Influence on Aircraft Tank Insulation

  • C. A. Schalla
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 12)


Hydrogen is making its appearance on the horizon of supersonic and hypersonic aircraft fuels. The expanding regimes of speed, altitude, and range of aircraft of the 1970’s will grow out of advances in many different technologies. However, hydrogen fuel will be the common design denominator.


Heat Transfer Coefficient Liquid Level Hydrogen Fuel Tank Model Tank Bottom 
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    B. L. Messinger, “Thermal Management of Lockheed Model 2000 Supersonic Transport,” ASME Paper No. 65-AV-40 (March 1965).Google Scholar
  2. 2.
    H. A. Berdelman, “Thermal Stresses in the Composite Wall of a Cryogenic Tank,” ASME Paper No. 65-AV-6 (March 1965).Google Scholar
  3. 3.
    R. T. Parmley and J. J. Brogan, Handbook of Thermal Design Data for Multilayer Insulation Systems, LMSC A742593 (August 11, 1965).Google Scholar
  4. 4.
    H. O. Croft, Thermodynamics, Fluid Flow and Heat Transmission, McGraw-Hill Book Co., New York (1938).Google Scholar
  5. 5.
    “Thermal Protection for Liquid-Hydrogen Fuel Tanks in High-Speed Long-Range Aircraft,” RAND Corporation, AD-625 407 (October 1965).Google Scholar

Copyright information

© Springer Science+Business Media New York 1967

Authors and Affiliations

  • C. A. Schalla
    • 1
  1. 1.Lockheed Missiles & Space CompanySunnyvaleUSA

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