The Goddard Space Flight Center mechanical cooler program

Details The Goddard Space Flight Center mechanical cooler program The Goddard Space Flight Center mechanical cooler program

Sep 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987cfmt.conf..377c&link_type=abstract

In NASA. Lewis Research Center, Cleveland, Ohio. Cryogenic Fluid Management Technology Workshop. Volume 1: Presentation Material

Astronomy and Astrophysics

Astrophysics

Brayton Cycle, Centrifugal Compressors, Coolers, Cryogenic Cooling, Cryogenic Equipment, Stirling Cycle, Turbomachinery, X Ray Astrophysics Facility, Heat Exchangers, Magnetic Suspension, Requirements

Scientific paper

The Philips Stirling Cooler Program will ensure that a cooler is available to meet NASA's needs in the 40 to 120K temperature range in the 1990's. The Creare turbomachinery based cooler may provide an improved cooler for the 40 to 120K range. The design of advanced multistage coolers for use down to 2K will begin in 1988. Requirements, the history of the Stirling cooler, features of the photoflight cooler, advantages of the Philips cooler, mechanical reliability, and potential advantages of the Creare reverse Brayton cycle cooler are presented in viewgraph form.

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