A computer simulation was performed to determine the design criteria for a spacelab refrigerator/freezer using the test results of a vapor compression refrigerator/freezer which flew on STS-4 without problem. It has been established to have a vapor Reynolds number over 3000 at a vapor quality of 0.2 to maintain annular boiling in the evaporator and for the condenser to have a vapor Reynolds number over 15000 at its inlet to maintain annular condensation. These two constraints will virtually eliminate the effect of gravity on the performance of the refrigerator/freezer. These results are being used to build a refrigerator/freezer which will fly in Spacelab-4 scheduled for launch in December 1985.
The design and development of a vapor compression refrigerator/freezer for spacelab
Konstruktion und Entwicklung eines Bruedenverdichterkuehlschranks und Frosters fuer Spacelab
SAE-Papers ; 1-8
1983
8 Seiten, 11 Bilder, 4 Tabellen, 25 Quellen
Aufsatz (Konferenz)
Englisch
The Design and Development of a Vapor Compression Refrigerator/Freezer for Spacelab
SAE Technical Papers | 1983
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AIAA | 1985
|Safety Considerations in the Design of Spacelab Refrigerator/Freezer
SAE Technical Papers | 1985
|The Design and Development of an Oil-Free Compressor for Spacelab Refrigerator/Freezer
SAE Technical Papers | 1984
|Shuttle Spacelab Core Equipment Freezer
AIAA | 1977
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