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Performance of Power Converters at Cryogenic TemperaturesPower converters capable of operation at cryogenic temperatures are anticipated to play an important role in the power system architecture of future NASA deep space missions. Design of such converters to survive cryogenic temperatures will improve the power system performance and reduce development and launch costs. Aerospace power systems are mainly a DC distribution network. Therefore, DC/DC and DC/AC converters provide the outputs needed to different loads at various power levels. Recently, research efforts have been performed at the NASA Glenn Research Center (GRC) to design and evaluate DC/DC converters that are capable of operating at cryogenic temperatures. This paper presents a summary of the research performed to evaluate the low temperature performance of five DC/DC converters. Various parameters were investigated as a function of temperature in the range of 20 to -196 C. Data pertaining to the output voltage regulation and efficiency of the converters is presented and discussed.
Document ID
20020011681
Acquisition Source
Jet Propulsion Laboratory
Document Type
Technical Memorandum (TM)
Authors
Elbuluk, Malik E.
(Akron Univ. Akron, OH United States)
Gerber, Scott
(ZIN Technologies, Inc. Brook Park, OH United States)
Hammoud, Ahmad
(QSS Group, Inc. Brook Park, OH United States)
Patterson, Richard L.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2001
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
E-12979
NAS 1.15:211130
NASA/TM-2001-211130
Meeting Information
Meeting: Eighth International Conference on Electronics, Circuits and Systems
Country: Malta
Start Date: September 2, 2001
End Date: September 5, 2001
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
PROJECT: RTOP 755-A4-12
CONTRACT_GRANT: NAS3-00145
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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