Skip to main content

Performance Testing of a Lightweight, High Efficiency Cooler

  • Chapter
Cryocoolers 12

Abstract

A lightweight, high efficiency cryocooler has been tested. The design operating point of the cooler is 10 W at 95 K with a rejection temperature of 300 K, and the goal is a 10 yr operating lifetime. The cooler has a mass of less than 4.0 kg. The cooler efficiency at the design operating point is 12.6 W/W. These values represent approximately a one-third decrease in mass and a one-third increase in efficiency over previous designs.

The pulse tube is built by TRW, and the compressor is built by Hymatic Engineering, UK. TRW integrates the compressor with the pulse tube and performs final testing of the assembly. Development of the cooler was performed by TRW under a joint NASA-DOD program.

Data presented were taken at controlled rejection temperatures of 285 K and 300 K using a cold-water heat exchanger bolted to the cooler. Heat loads were varied between 1W and 10 W by supplying current to a 25.6Ω resistor mounted on the cooler cold block. Input power to the compressor was limited to 180 W.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 169.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 219.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 219.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Salerno, L. J., Valentian, D., Plachta, D., Kittel, P., Hastings, L. J., “Zero Boil off Cryogen Storage for Future Launchers”, Proc. of the 3rd European Conference on Launcher Technology, Strasbourg, France, Dec 11–14, 2001, pp. 399

    Google Scholar 

  2. Hastings, L. J., Plachta, D., Salerno, L., and Kittel, P., “An Overview of NASA Efforts on Zero Boiloff Storage of Cryogenic Propellents”, presented at the Space Cryogenics Workshop, July 2001, Milwaukee, Wisconsin, Cryogenics, vol. 41, no.12, (2001), pp. 833–839

    Article  ADS  Google Scholar 

  3. Tward, E., Chan, C. K., Colbert, R., Jaco, C., Nguyen, T., Orsini, R., Raab, J., “High Efficiency Cryocooler”, Adv. in Cryo Eng, 47, American Institute of Physics, Melville, New York (2002), pp. 1077–1084

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2003 Kluwer Academic Publishers

About this chapter

Cite this chapter

Salerno, L.J., Kittel, P., Helvensteijn, B.P.M., Kashani, A. (2003). Performance Testing of a Lightweight, High Efficiency Cooler. In: Ross, R.G. (eds) Cryocoolers 12. Springer, Boston, MA. https://doi.org/10.1007/0-306-47919-2_27

Download citation

  • DOI: https://doi.org/10.1007/0-306-47919-2_27

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-0-306-47714-0

  • Online ISBN: 978-0-306-47919-9

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics