DocumentCode
2509594
Title
Extended life interconnect for large solar cell space arrays
Author
Gaddy, Edward M.
Author_Institution
Solarex Aerosp. Div., Rockville, MD, USA
fYear
1988
fDate
1988
Firstpage
964
Abstract
Calculations are presented that show that the stress in this interconnect is reduced by a factor of 60 as compared to interconnects that make use of only the intercell spacing for their stress relief loop. The reason is that traditional interconnects use only an intercell spacing of about 0.5 mm to absorb stress. The extended life interconnect positions the stress interconnect member parallel to the gap between the cells. Therefore, the interconnect´s stressed member can be much longer and the stress consequently less. Also presented are the results of mechanically cycling the interconnect.
Keywords
solar cell arrays; solar cells; space vehicle power plants; testing; extended life interconnect; intercell spacing; large solar cell space arrays; stress relief loop; Aircraft manufacture; Aluminum; Assembly; Elasticity; Equations; Photovoltaic cells; Space vehicles; Stress; Temperature distribution; Thermal expansion; Thermal stresses;
fLanguage
English
Publisher
ieee
Conference_Titel
Photovoltaic Specialists Conference, 1988., Conference Record of the Twentieth IEEE
Conference_Location
Las Vegas, NV, USA
Type
conf
DOI
10.1109/PVSC.1988.105848
Filename
105848
Link To Document