DocumentCode
2613712
Title
In-flight performance of the SBS-1A solar array featuring ultrathin, high efficiency solar cells
Author
Williams, R.D. ; Gelb, S.W. ; Fodor, J.S.
Author_Institution
Hughes Aircraft Co., Los Angeles, CA, USA
fYear
1990
fDate
21-25 May 1990
Firstpage
1226
Abstract
Ultrathin (0.0025 in.) Si solar cells were selected for use on the Satellite Business System (SBS) 1A solar array to achieve minimum solar array weight and maximum end-of-life solar array power. The design of the ultrathin cell was predicted to produce an improved resistance to radiation degradation and superior current collection efficiency, thus increasing the power per unit area at end of life compared to conventional-thickness silicon solar cells. The ultrathin solar cells were qualified for flight and characterized prior to fabrication of the SBS-1A array. Performance predictions in the mission environment were based on these characteristics and on the measured photovoltaic output of the flight solar cells. The predicted solar array performance has been validated to date within 2% by in-flight test data
Keywords
elemental semiconductors; silicon; solar cell arrays; space vehicle power plants; 0.0025 inch; SBS-1A solar array; Satellite Business System; Si solar cells; high efficiency; in-flight test; radiation degradation resistance; ultrathin cell; Aircraft; Artificial satellites; Assembly; Batteries; Business communication; Companies; Degradation; Photovoltaic cells; Silicon; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Photovoltaic Specialists Conference, 1990., Conference Record of the Twenty First IEEE
Conference_Location
Kissimmee, FL
Type
conf
DOI
10.1109/PVSC.1990.111810
Filename
111810
Link To Document