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Refractory metal alloys and composites for space power systemsSpace power requirements for future NASA and other U.S. missions will range from a few kilowatts to megawatts of electricity. Maximum efficiency is a key goal of any power system in order to minimize weight and size so that the space shuttle may be used a minimum number of times to put the power supply into orbit. Nuclear power has been identified as the primary source to meet these high levels of electrical demand. One way to achieve maximum efficiency is to operate the power supply, energy conversion system, and related components at relatively high temperatures. NASA Lewis Research Center has undertaken a research program on advanced technology of refractory metal alloys and composites that will provide baseline information for space power systems in the 1900's and the 21st century. Basic research on the tensile and creep properties of fibers, matrices, and composites is discussed.
Document ID
19880017926
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stephens, Joseph R.
(NASA Lewis Research Center Cleveland, OH, United States)
Petrasek, Donald W.
(NASA Lewis Research Center Cleveland, OH, United States)
Titran, Robert H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.15:100946
NASA-TM-100946
E-4237
Report Number: NAS 1.15:100946
Report Number: NASA-TM-100946
Report Number: E-4237
Accession Number
88N27310
Funding Number(s)
PROJECT: RTOP 586-01-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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