Epoxy-Nylon Adhesives for Low-Temperature Applications

  • J. Hertz
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 7)

Abstract

Because of the extensive use of liquid oxygen and liquid hydrogen In both present and future space vehicles It has become necessary to obtain adhesives which will retain structural strengths at temperatures as low as -423°F. The Centaur vehicle is now utilizing adhesives for bonding plastic foam Insulation to a stainless steel tank, for bonding plastic honeycomb sandwich panels, and for bonding Mylar to stainless steel tanks. These adhesive bonds must withstand operating temperatures of -423°F, Future vehicles will have many more cryogenic applications which will require adhesive bonding. These applications may vary from the bonding of small clips to cryogen tanks to the problem of manufacturing full-scale, adhesive-bonded metal tanks.

Keywords

Shear Strength Impact Specimen Stainless Steel Tank Average Bond Strength Composite Sandwich Structure 
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.
    J. Hertz, “Structural Adhesives for Cryogenic Applications,”Adhesives Age (August, 1961).Google Scholar
  2. 2.
    J.F. Watson and J.L. Christian, “Cryostat and Accessories for Tension Testing at -423°F,” Material Research & Standards, Vol. I, No. 3 (February, 1961).Google Scholar
  3. 3.
    J. Lincoln and B. Smith, Manufacturer’s Literature, Narmco Research and Development, Telecomputing Corporation (1961).Google Scholar
  4. 4.
    W. M. Frost, “Strengths of Structural Adhesives at Temperatures Down to Minus 424°F,” Cryogenic Engineering Laboratory, National Bureau of Standards, WADC Technical Report 59–260 (April, 1959).Google Scholar
  5. 5.
    Astia Document No. 151529, “Adhesives Properties, -300° to +700°F,” North American Aviation.Google Scholar
  6. 6.
    R.M. McClintock and M.J. Hiza, “Epoxy Resins as Cryogenic Structural Adhesives” Modern Plastics (June, 1958).Google Scholar
  7. 7.
    J. Hertz, “Tensile Testing of Adlock 851, Adlock PG-LA and Adlock EG-11A-81A from -423°F to 78°F,” General Dynamics/Astronautics Report No. MRG-237 (June, 1961).Google Scholar

Copyright information

© Springer Science+Business Media New York 1962

Authors and Affiliations

  • J. Hertz
    • 1
  1. 1.General Dynamics/AstronauticsSan DiegoUSA

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