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Low-temperature Brayton radiator performance in a variable-sink-temperature environmentAn analysis of the performance of a low-temperature Brayton space radiator is presented. The cylindrical radiator with circumferential tubes was subjected to an equivalent sink temperature environment that varied along the fluid flow path. The radiator performance, as measured by fluid outlet temperature, was found to be dependent on the orbital position and the location of the radiator inlet relative to the sink temperature environment. An approximate dynamic analysis of sun-shade variations in performance is included.
Document ID
19720005297
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bien, D. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
E-6561
NASA-TM-X-2450
Report Number: E-6561
Report Number: NASA-TM-X-2450
Accession Number
72N12946
Funding Number(s)
PROJECT: RTOP 112-27
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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