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Design of large, low-concentration-ratio solar arrays for low earth orbit applications

Conference · · Proc., Intersoc. Energy Convers. Eng. Conf.; (United States)
OSTI ID:5355091
This paper describes an ongoing preliminary design effort directed toward a low-concentration-ratio photovoltaic array based on 1984 technology and capable of delivering several hundred kilowatts of electrical power in low earth orbit. The array consists of rectangular modules of about 1,400 square meters in area, each consisting of approximately 4,400 pyramidal concentrator elements. The modules are stored in the Space Shuttle's payload bay as cubes (3.24 meters on a side) and are deployed and extended in orbit by means of canister/mast assemblies. The concentrator elements are sized for a geometric concentration ratio (GCR) of six and may be used either with silicon (Si) or gallium arsenide (GaAs) solar cells. The paper discusses the structural analysis and design trades leading to the baseline design. It also describes the optical, thermal and electrical performance analyses that support the design and provide overall performance estimates for the array.
Research Organization:
Rockwell International Corp., Seal Beach, CA
OSTI ID:
5355091
Report Number(s):
CONF-820814-
Conference Information:
Journal Name: Proc., Intersoc. Energy Convers. Eng. Conf.; (United States) Journal Volume: 3
Country of Publication:
United States
Language:
English