Abstract
Introduction of multilayer insulation (MLI) in the late 1950’s had an immediate impact on the cryogenic community. There was a flurry of activity on the part of manufacturers and laboratories to learn how to utilize and evaluate this dramatic improvement in insulation technology. However, by the late 1960’s, MLI had become a generic term for multiple reflector material with and without separators and most laboratories had moved on to other work. Although knowledge of MLI was certainly not complete, it was sufficient for construction of low heat leak dewars and cryogenic apparatus. As the experience base grew, empirical MLI design equations began to appear with some, in particular the “Lockheed”1 equation, capable of accurately predicting performance of certain combinations of reflector and separator materials. Fortunately, there were individuals who realized that MLI technology was not complete and were able to obtain funding to support continued development. In this category, recognition should be given to Dr. Ron Fast2 and his associates at Fermilab, Mr. T. C. Nast3 and associates at Lockheed, and, more recently, Mr. W. N. Boroski4 who has been working at Fermilab on behalf of the SSC.
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References
C.W. Keller, G.R. Cunnington and A.P. Glassford, “Final Report-Thermal Performance of Multilayer Insulations,” NASA CR-134477 (April 1974).
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© 1994 Springer Science+Business Media New York
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McIntosh, G.E. (1994). Layer by Layer MLI Calculation Using a Separated Mode Equation. In: Kittel, P. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 39. Springer, Boston, MA. https://doi.org/10.1007/978-1-4615-2522-6_206
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DOI: https://doi.org/10.1007/978-1-4615-2522-6_206
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