Cryocoolers 8 pp 103-112 | Cite as

30 K Diaphragm Stirling Cryocooler Demonstration

  • W. D. Stacy
  • W. R. Baschnagel
  • D. B. Lussier

Abstract

This paper describes an Engineering Model cryocooler of two-stage Stirling type and metal diaphragm construction which has been delivered to NASA Goddard Space Flight Center. The unit provides 269 milliwatts of net cooling at 30 K. Key design features are described, and performance results are presented for capacity and power. Vibration and life testing at Goddard have been initiated.

Keywords

Electron Beam Welding Engineer Model Expander Pressure NASA Goddard Space Cold Expander 
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.
    Stacy, W.D. A 10 Year Life 65 K Stirling Cryocooler for Satellite Sensor Applications, 6th Inter-Agency Cryocooler Conference, Plymouth, MA, Oct. 24, 1990.Google Scholar
  2. 2.
    Stacy, W.D., McCormick, J.A., and Valenzuela, J.A.; Development and Demonstration of a Diaphragm Stirling 65 K Standard Spacecraft Cryocooler, 7th International Cryocooler Conf., Oct. 7, 1992.Google Scholar
  3. 3.
    Konkel, C., Gibboney, T., VanAllen, L, Ha, K, Boyle, R; Development and Demonstration of an Electronics Controller for a Double-Acting Diaphragm Cooler, 7th International Cryocooler Conference, Nov. 1992.Google Scholar
  4. 4.
    Konkel, C., Gibboney, T., Ha, K., Boyle, R.; Implementation and Test of the Control Algorithm for a Diaphragm Stirling 30 K Cryocooler; 8th International Cryocooler Conference, June 1994.Google Scholar

Copyright information

© Springer Science+Business Media New York 1995

Authors and Affiliations

  • W. D. Stacy
    • 1
  • W. R. Baschnagel
    • 1
  • D. B. Lussier
    • 2
  1. 1.Creare Inc.HanoverUSA
  2. 2.Fairchild SpaceGreenbeltUSA

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