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Thermal management considerations for 100 kW(e) In-Core Thermionic Space Nuclear Power SystemThe general thermal management approach for the SP-100 In-Core Thermionic Space Nuclear Power System is presented. Thermal advantages and design features of the heat transport subsystem are addressed, including the selection of parameters, heat transport fluid, and materials. Pumping considerations, thermal insulation requirements, and radiator design are discussed, and the impacts of system scaling to higher power levels are projected.
Document ID
19840055268
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Van Hagan, T. H.
(GA Technologies, Inc. San Diego, CA, United States)
Campana, R. J.
(GA Technologies, Inc. San Diego, CA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 84-1755
Report Number: AIAA PAPER 84-1755
Accession Number
84A38055
Funding Number(s)
CONTRACT_GRANT: JPL-956472
Distribution Limits
Public
Copyright
Other

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