DocumentCode
2562226
Title
Advanced Photovoltaic Solar Array Program status
Author
Kurland, Richard M. ; Stella, Paul M.
Author_Institution
TRW, Redondo Beach, CA, USA
fYear
1989
fDate
6-11 Aug 1989
Firstpage
829
Abstract
The Advanced Photovoltaic Solar Array (APSA) Program for spacecraft is discussed. The objective of the program is to demonstrate a producible array system by the end of this decade with a beginning-of-life (BOL) specific power of 130 W/kg at 10 kW as an intermediate milestone toward the ultimate goal of 300 W/kg at 25 kW by the year 2000. The near-term goal represents a significant improvement over existing rigid panel flight arrays (25 to 45 W/kg) and the first-generation flexible blanket NASA/OAST SAFE I array of the early 1980s, which was projected to provide about 60 W/kg BOL. The prototype wing hardware is in the last stages of fabrication and integration. The current status of the program is reported. The array configuration and key design details are shown. Projections are shown for future performance enhancements that may be expected through the use of advanced structural components and solar cells
Keywords
solar cell arrays; space vehicle power plants; Photovoltaic Solar Array Program; beginning-of-life specific power; solar cells; Gold; Hardware; Laboratories; NASA; Photovoltaic systems; Propulsion; Prototypes; Solar power generation; Space technology; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
Conference_Location
Washington, DC
Type
conf
DOI
10.1109/IECEC.1989.74565
Filename
74565
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