Skip to main content

Development of Pulse Tube Cryocoolers for HTS Satellite Communications

  • Chapter
Cryocoolers 10

Abstract

The Advanced Technology Center of Lockheed Martin is developing high-capacity (10 W @ 77 K) and low-capacity (0.5 W @ 77 K) pulse tube cryocoolers as part of a program to develop reduced weight satellite communications payloads utilizing high-temperature superconducting (HTS) microwave circuits. A consortium of Com Dev, DuPont, and Lockheed Martin is working together with NASA Lewis Research Center to develop this technology under a DARPA program.

The cooling performance and system characteristics of both the high-power and low power cryocooler systems are described in this paper.

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. Kotsubo, V., Olson, J, R., and Nast, T. C., “Development of a 2 W @ 60 K Pulse Tube Cryocooler for Spacebome Operation,” these proceedings.

    Google Scholar 

  2. Nast, T., Champagne, P, and Kotsubo, V, “Development of a Low-cost Unlimited-life Pulse Tube Cryocooler for Commercial Applications,” to be published in Adv. Cryo. Engin.

    Google Scholar 

  3. Nast, T. C., Champagne, P.J., Isaac, D., Pryor, G. M., von Savoye, R. L. and Naes, L. G., “Design, Performance and Testing of the Lockheed-Developed Mechanical Cryocooler,” Proc. 8th International Cryocooler Conference, Vail, CO (1994).

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2002 Kluwer Academic Publishers

About this chapter

Cite this chapter

Kotsubo, V., Olson, J., Champagne, P., Williams, B., Clappier, B., Nast, T.C. (2002). Development of Pulse Tube Cryocoolers for HTS Satellite Communications. In: Ross, R.G. (eds) Cryocoolers 10. Springer, Boston, MA. https://doi.org/10.1007/0-306-47090-X_19

Download citation

  • DOI: https://doi.org/10.1007/0-306-47090-X_19

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-0-306-46120-0

  • Online ISBN: 978-0-306-47090-5

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics