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Radiator design system computer programsMinimum weight space radiator subsystems which can operate over heat load ranges wider than the capabilities of current subsystems are investigated according to projected trends of future long duration space vehicles. Special consideration is given to maximum heat rejection requirements of the low temperature radiators needed for environmental control systems. The set of radiator design programs that have resulted from this investigation are presented in order to provide the analyst with a capability to generate optimum weight radiator panels or sets of panels from practical design considerations, including transient performance. Modifications are also provided for existing programs to improve capability and user convenience.
Document ID
19730015219
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wiggins, C. L.
(Vought Missiles and Space Co. Dallas, TX, United States)
Oren, J. A.
(Vought Missiles and Space Co. Dallas, TX, United States)
Dietz, J. B.
(Vought Missiles and Space Co. Dallas, TX, United States)
Date Acquired
September 2, 2013
Publication Date
October 13, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-128913
Report Number: NASA-CR-128913
Accession Number
73N23946
Funding Number(s)
CONTRACT_GRANT: NAS9-10810
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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