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Advanced radiator conceptsTwo radiator systems to reject heat from future space nuclear power systems were conceptually designed. One design would dissipate 1.7 MWt of heat at 600 K, and the other would reject 2.4 MWt at 875 K. The low-temperature radiator utilized a pumped loop system constructed of titanium, and achieved a specific mass of 5.8 kg/sq m, including pumps and structure. The high-temperature radiator system utilized potassium heat pipes constructed of SiC-reinforced titanium, and achieved a specific mass of 5.5 kg/sq m. Both radiators took advantage of light, high-thermal-conductivity carbon/graphite composite fins to distribute and radiate the rejected heat.
Document ID
19900050987
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Begg, L. L.
(Space Power, Inc. San Jose, CA, United States)
Engdahl, E. H.
(Space Power, Inc. San Jose, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: IECEC-89
Location: Washington, DC
Country: United States
Start Date: August 6, 1989
End Date: August 11, 1989
Accession Number
90A38042
Funding Number(s)
CONTRACT_GRANT: NAS3-25208
Distribution Limits
Public
Copyright
Other

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