Actions for 1987 Overview of the free-piston Stirling technology for space power application [electronic resource].

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1987 Overview of the free-piston Stirling technology for space power application [electronic resource].

Published
Washington, D.C. : United States. Dept. of Energy, 1994.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy.
Physical Description
12 pages : digital, PDF file
Additional Creators
Lewis Research Center, United States. Department of Energy, and United States. Department of Energy. Office of Scientific and Technical Information
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Summary
An overview is presented of the National Aeronautics and Space Administration (NASA) Lewis Research Center free-piston Stirling engine activities directed toward space-power application. Free-piston Stirling technology is applicable for both solar and nuclear powered systems. As such, NASA Lewis serves as the project office to manage the newly initiated NASA SP-100 Advanced Technology Program. This 5-yr program provides the technology thrust for providing significant component and subsystem options for increased efficiency, reliability and survivability, and power output growth at reduced specific mass. One of the major elements of the program is the development of advanced power conversion concepts of which the Stirling cycle is a viable growth candidate. Under this program the status of the 25 kWe opposed-piston Space Power Demonstrator Engine (SPDE) is presented. Included in the SPDE discussion are comparisons between predicted and experimental engine performance, enhanced performance resulting from regenerator modification, increased operating stroke brought about by isolating the gas bearing flow between the displacer and power piston, identifying excessive energy losses and recommending corrective action, and a better understanding of linear alternator design and operation. Technology work is also conducted on heat exchanger concepts, both design and fabrication, to minimize the number of joints as well as to enhance performance. Design parameters and conceptual design features are also presented for a 25 kWe, single-cylinder free-piston Stirling space-power converter. A cursory comparison is presented showing the mass benefits that a Stirling system has over a Brayton system for the same peak temperature and output power.
Report Numbers
E 1.99:nasa-tm--89832
E 1.99: conf-870804--53
conf-870804--53
nasa-tm--89832
Subject(s)
Other Subject(s)
Note
Published through SciTech Connect.
09/01/1994.
"nasa-tm--89832"
" conf-870804--53"
"DE94051259"
22. intersociety energy conversion engineering conference,Philadelphia, PA (United States),10-14 Aug 1987.
Slaby, J.G.; Alger, D.L.
Funding Information
AI03-86SF16310
View MARC record | catkey: 13600689