Design, Performance, and Testing of the Lockheed-Developed Mechanical Cryocooler

  • T. C. Nast
  • P. J. Champagne
  • D. Isaac
  • G. M. Pryor
  • R. L. von Savoye
  • L. G. Naes

Abstract

Lockheed has developed a split-Stirling cycle common compression space cryocooler that provides more than 1.5-W cooling at 55 K, while drawing less than 50 W/W into the compressors. The design improves on the flexure spring and gas-gap seal design originally developed by Oxford University. Significant design improvements have been incorporated in the compressor and displacer, yielding improved cooling and efficiency, resulting in the measured performance achieved to date.

A description of the Lockheed Model L-1710C cryocooler and a summary of its performance and environmental test program are presented next.

Keywords

Heat Load Active Balancer Load Line Cold Finger Residual Vibration 
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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Copyright information

© Springer Science+Business Media New York 1995

Authors and Affiliations

  • T. C. Nast
    • 1
  • P. J. Champagne
    • 1
  • D. Isaac
    • 1
  • G. M. Pryor
    • 1
  • R. L. von Savoye
    • 1
  • L. G. Naes
    • 1
  1. 1.Research & Development DivisionLockheed Missiles & Space Company, Inc.Palo AltoUSA

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