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NASA NTRS ยท 19730023260

Analysis of a combined refrigerator-generator space power system

Abstract

Compatibility of the Brayton power and refrigeration cycles is considered. Performance of the power- and cryo-loop is plotted against compressor pressure ratio. The power- and cryo-loop performance is determined by dividing the compressor work between the two loops in proportion to mass flow rate. Cycle efficiency is defined as the ratio of shaft power available in the power loop to the net thermal input from the heat source. The available shaft power is the excess of the power turbine work over the compressor work needed in the power loop. The best power loop efficiency occurred at a compressor pressure ratio of 1.8, and the best cryo-loop performance was at a compressor pressure ratio of 2.1. Good individual cycle performance occurred over a fairly large range in compressor pressure ratio.

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BibTeXRIS

Klann, J. L.. 1973-01-01. Analysis of a combined refrigerator-generator space power system. https://ntrs.nasa.gov/citations/19730023260

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