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Sizing-tube-fin space radiatorsTemperature and size considerations of the tube fin space radiator were characterized by charts and equations. An approach of accurately assessing rejection capability commensurate with a phase A/B level output is reviewed. A computer program, based on Mackey's equations, is also presented which sizes the rejection area for a given thermal load. The program also handles the flow and thermal considerations of the film coefficient.
Document ID
19780022606
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Peoples, J. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-78185
Report Number: NASA-TM-78185
Accession Number
78N30549
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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