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Spaceborne power systems preference analyses. Volume 2: Decision analysisSixteen alternative spaceborne nuclear power system concepts were ranked using multiattribute decision analysis. The purpose of the ranking was to identify promising concepts for further technology development and the issues associated with such development. Four groups were interviewed to obtain preference. The four groups were: safety, systems definition and design, technology assessment, and mission analysis. The highest ranked systems were the heat-pipe thermoelectric systems, heat-pipe Stirling, in-core thermionic, and liquid-metal thermoelectric systems. The next group contained the liquid-metal Stirling, heat-pipe Alkali Metal Thermoelectric Converter (AMTEC), heat-pipe Brayton, liquid-metal out-of-core thermionic, and heat-pipe Rankine systems. The least preferred systems were the liquid-metal AMTEC, heat-pipe thermophotovoltaic, liquid-metal Brayton and Rankine, and gas-cooled Brayton. The three nonheat-pipe technologies selected matched the top three nonheat-pipe systems ranked by this study.
Document ID
19850016207
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, J. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Feinberg, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Miles, R. F., Jr.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
January 15, 1985
Subject Category
Energy Production And Conversion
Report/Patent Number
NAS 1.26:175645
JPL-PUB-85-5-VOL-2
NASA-CR-175645
Report Number: NAS 1.26:175645
Report Number: JPL-PUB-85-5-VOL-2
Report Number: NASA-CR-175645
Accession Number
85N24518
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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