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NASA NTRS · 20040068202

Cryocoolers for Space

Abstract

Many planetary and Earth science missions require cooling to increase sensitivity and reduce thermal noise of detectors, for preserving high Isp propellants, or for protecting instruments from hostile environments. For space applications, such cooling requires reliable, efficient, long-life coolers that are relatively compact, lightweight, and have low vibration. We have developed and are developing coolers that meet these requirements over a wide range of temperatures. These include pulse tube coolers cooling from 300 K to below 6 K, a magnetic cooler cooling from 10 K to 2 K, a 3He sorption cooler cooling from 2 K to 0.3 K and a helium dilution cooler cooling from 0.3 K to 0.05 K. Details of these coolers and their advantages are presented.

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BibTeXRIS

Kittel, Peter, Feller, Jeff, Roach, Pat, Kashani, Ali, Helvensteijn, Ben. 2004-02-01. Cryocoolers for Space. https://ntrs.nasa.gov/citations/20040068202

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