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Performance of the Oxford Miniature Stirling Cycle Refrigerator

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Advances in Cryogenic Engineering

Part of the book series: Advances in Cryogenic Engineering ((ACRE,volume 31))

Abstract

The performance of the Oxford Cryocooler is summarised. This cooler has been developed for space use by the Rutherford Appleton Laboratory and the Departments of Atmospheric Physics and Engineering Science at Oxford University. The design goal of 1/2 watt of cooling power at 80 K for 30 W electrical input power has been exceeded by a substantial amount. The power budget for the compressor and the losses in the displacer are discussed. Graphs of the cold end temperature vs. compressor input power and cooling power are presented.

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References

  1. S.T. Werrett et al., Development of a small Stirling cycle cooler for spaceflight applications,in:“Advances in Cryogenic Engineering”, Vol.31, Plenum Press,New York (1986).

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© 1986 Plenum Press, New York

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Bradshaw, T.W., Delderfield, J., Werrett, S.T., Davey, G. (1986). Performance of the Oxford Miniature Stirling Cycle Refrigerator. In: Fast, R.W. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 31. Springer, Boston, MA. https://doi.org/10.1007/978-1-4613-2213-9_90

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  • DOI: https://doi.org/10.1007/978-1-4613-2213-9_90

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4612-9299-9

  • Online ISBN: 978-1-4613-2213-9

  • eBook Packages: Springer Book Archive

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