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Advanced photovoltaic solar array design assessmentThe Advanced Photovoltaic Solar Array (APSA) program seeks to bring to flight readiness a solar array that effectively doubles the specific power of the Solar Array Flight Experiment/Solar Electric Propulsion (SAFE/SEP) design that was successfully demonstrated during the Shuttle 41-D mission. APSA is a critical intermediate milestone in the effort to demonstrate solar array technologies capable of 300 W/kg and 300 W/square m at beginning of life (BOL). It is not unreasonable to anticipate the development of solar array designs capable of 300 W/kg at BOL for operational power levels approx. greater than 25 kW sub e. It is also quite reasonable to expect that high performance solar arrays capable of providing at least 200 W/kg at end of life for most orbits now being considered by mission planners will be realized in the next decade.
Document ID
19870016996
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stella, Paul
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Scott-Monck, John
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1987
Publication Information
Publication: NASA. Lewis Research Center, Space Photovoltaic Research and Technology 1986. High Efficiency, Space Environment and Array Technology
Subject Category
Energy Production And Conversion
Accession Number
87N26429
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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