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Evaluation and selection of refrigeration systems for lunar surface and space applicationsEvaluated are the various refrigeration machines which could be used to provide heat rejection in environmental control systems for lunar surface and spacecraft applications, in order to select the best refrigeration machine for satisfying each individual application and the best refrigeration machine for satisfying all of the applications. The refrigeration machine considered include: (1) vapor comparison cycle (work-driven); (2) vapor adsorption cycle (heat-driven); (3) vapor absorption cycle (heat-driven); (4) thermoelectric (electrically-driven); (5) gas cycle (work driven); (6) steam-jet (heat-driven).
Document ID
19720009283
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Copeland, R. J.
(Vought Missiles and Space Co. Dallas, TX, United States)
Blount, T. D.
(Vought Missiles and Space Co. Dallas, TX, United States)
Williams, J. L.
(Vought Missiles and Space Co. Dallas, TX, United States)
Date Acquired
September 2, 2013
Publication Date
October 31, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
T122RP04
NASA-CR-115352
Accession Number
72N16933
Funding Number(s)
CONTRACT_GRANT: NAS9-9912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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