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Electrical power system design for the US space stationThe multipurpose, manned, permanent space station will be our next step toward utilization of space. A multikilowatt electrical power system will be critical to its success. The power systems for the space station manned core and platforms that have been selected in definition studies are described. The system selected for the platforms uses silicon arrays and Ni-H2 batteries. The power system for the manned core is a hybrid employing arrays and batteries identical to those on the platform along with solar dynamic modules using either Brayton or organic Rankine engines. The power system requirements, candidate technologies, and configurations that were considered, and the basis for selection, are discussed.
Document ID
19870005834
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nored, Donald L.
(NASA Lewis Research Center Cleveland, OH, United States)
Bernatowicz, Daniel T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
August 29, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-3073
NASA-TM-88824
NAS 1.15:88824
Report Number: E-3073
Report Number: NASA-TM-88824
Report Number: NAS 1.15:88824
Accession Number
87N15267
Funding Number(s)
PROJECT: RTOP 485-49-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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