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Design point characteristics of a 500 - 2500 watt isotope-Brayton power system.An analytical study was conducted to investigate the potential performance characteristics of an isotope-Brayton space power system at electric power levels from 500 to 2500 W. Utilization of the Pu 238 heat source, or capsule, being developed for the Multi-Hundred Watt Radioisotope Thermoelectric Generator was assumed. A single-loop system design concept was selected. The design concept and results of first-order tradeoff studies of the effects of major system parameters on system performance are presented. Results of the study indicate the potential for high system efficiency and high specific power over the entire power range.
Document ID
19730028586
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barna, G. J.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Subject Category
Auxiliary Systems
Report/Patent Number
AIAA PAPER 72-1059
Meeting Information
Meeting: Joint Propulsion Specialist Conference
Location: New Orleans, LA
Country: US
Start Date: November 29, 1972
End Date: December 1, 1972
Sponsors: American Institute of Aeronautics and Astronautics, Society of Automotive Engineers
Accession Number
73A13388
Distribution Limits
Public
Copyright
Other

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