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Evaluation of absorption cycle for space station environmental control system applicationThe study to evaluate an absorption cycle refrigeration system to provide environmental control for the space stations is reported. A zero-gravity liquid/vapor separator was designed and tested. The results were used to design a light-weight, efficient generator for the absorption refrigeration system. It is concluded that absorption cycle refrigeration is feasible for providing space station environmental control.
Document ID
19730006132
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sims, W. H. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Oneill, M. J. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Reid, H. C. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Bisenius, P. M. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
LMSC/HREC-D306225
NASA-CR-123970
HREC-5986-2
Report Number: LMSC/HREC-D306225
Report Number: NASA-CR-123970
Report Number: HREC-5986-2
Accession Number
73N14859
Funding Number(s)
CONTRACT_GRANT: NAS8-25986
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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