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The ground testing of a 2 kWe solar dynamic space power systemThe solar dynamic power system chosen by NASA for Space Station Freedom SSF requires validation in the vacuum/microgravity environment. The planned ground tests of a proof-of-concept 2 kWe solar dynamic system with address subsystem integration issues involving such major system components as the behavior of thermal energy storage materials. This test scheme will be scalable to 25 kWe, and will be flight-configured to incorporate features of the SSF's power module design.
Document ID
19930041921
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Calogeras, James E. (NASA Lewis Research Center Cleveland, OH, United States)
Dustin, Miles O. (Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: IECEC '92; Proceedings of the 27th Intersociety Energy Conversion Engineering Conference, San Diego, CA, Aug. 3-7, 1992. Vol. 1 (A93-25851 09-44)
Publisher: Society of Automotive Engineers, Inc.
Subject Category
Spacecraft Propulsion And Power
Accession Number
93A25918
Distribution Limits
Public
Copyright
Other

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