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OAO-3 end of mission power subsystem evaluationEnd of mission tests were performed on the OAO-3 power subsystem in three component areas: solar array, nickel-cadmium batteries and the On-Board Processor (OBP) power boost operation. Solar array evaluation consisted of analyzing array performance characteristics and comparing them to earlier flight data. Measured solar array degradation of 14.1 to 17.7% after 8 1/3 years is in good agreement with theortical radiation damage losses. Battery discharge characteristics were compared to results of laboratory life cycle tests performed on similar cells. Comparison of cell voltage profils reveals close correlation and confirms the validity of real time life cycle simulation. The successful operation of the system in the OBP/power boost regulation mode demonstrates the excellent life, reliability and greater system utilization of power subsystems using maximum power trackers.
Document ID
19830003310
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Tasevoli, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-TM-83959
NAS 1.15:83959
Report Number: NASA-TM-83959
Report Number: NAS 1.15:83959
Meeting Information
Meeting: IECEC
Location: Los Angeles
Start Date: August 8, 1982
End Date: August 13, 1982
Accession Number
83N11580
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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