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Heat pipe reactors for space power applicationsA family of heat pipe reactors design concepts has been developed to provide heat to a variety of electrical conversion systems. Three power plants are described that span the power range 1-500 kWe and operate in the temperature range 1200-1700 K. The reactors are fast, compact, heat-pipe cooled, high-temperature nuclear reactors fueled with fully enriched refractory fuels, UC-ZrC or UO2. Each fuel element is cooled by an axially located molybdenum heat pipe containing either sodium or lithium vapor. Virtues of the reactor designs are the avoidance of single-point failure mechanisms, the relatively high operating temperature, and the expected long lifetimes of the fuel element components.
Document ID
19770041058
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Koenig, D. R.
(Los Alamos Scientific Lab. NM, United States)
Ranken, W. A.
(Los Alamos Scientific Lab. NM, United States)
Salmi, E. W.
(California, University Los Alamos, N. Mex., United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1977
Subject Category
Energy Production And Conversion
Report/Patent Number
AIAA PAPER 77-491
Meeting Information
Meeting: Conference on the Future of Aerospace Power Systems
Location: St. Louis, MO
Start Date: March 1, 1977
End Date: March 3, 1977
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A23910
Distribution Limits
Public
Copyright
Other

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