DocumentCode
440092
Title
Thermal cycle testing of GaAs on Si and metamorphic tandem on Si solar cells
Author
Wilt, David M. ; Pal, AnnaMaria T. ; Prokop, Norman F. ; Ringel, Steven A. ; Andre, Carrie L. ; Smith, Mark A. ; Scheiman, David A. ; Jenkins, Phillip P. ; Maurer, William F. ; McElroy, Bruce ; Fitzgerald, Eugene A.
Author_Institution
NASA Glenn Res. Center, Cleveland, OH, USA
fYear
2005
fDate
3-7 Jan. 2005
Firstpage
571
Lastpage
574
Abstract
GaAs on Si (GaAs/Si) solar cells grown on Si substrates coated with a step graded buffer of SixGe1-x alloys graded to 100% Ge have demonstrated AM0 efficiencies in excess of 17%. Recently, 4 cm2 devices were developed in preparation for on-orbit testing aboard Materials International Space Station Experiment number 5 (MISSES). In preparation for flight, thermal cycling life testing and thermal shock testing have been conducted to examine the stability of these thermal coefficient of expansion mismatched structures. Six thousand (6000) thermal cycles, equivalent to one year in LEO, from -80°C to +80°C have been completed with no discernable degradation in the electrical performance. The use of metamorphic III-V materials, of larger lattice parameter, has demonstrated the ability to dramatically reduce the micro crack density, presumably through strain balancing. Recently, the first demonstration of metamorphic tandem devices (1.6 eV InGaP / 1.1 eV InGaAs) on Si substrates was accomplished. The devices appeared micro crack free as determined by Nomarski optical microscopic examination and electroluminescence image analysis. Thermal shock testing of GaAs/Si devices showed micro crack formation and device electrical degradation. Thermal cycle testing of metamorphic structures (InGaP/InGaAs/Si) demonstrated a general lack of micro crack formation and improved thermal stability compared to GaAs/Si control devices.
Keywords
III-V semiconductors; aerospace testing; electroluminescence; elemental semiconductors; gallium arsenide; indium compounds; lattice constants; life testing; mechanical testing; microcracks; optical microscopy; semiconductor device testing; silicon; solar cells; space power generation; thermal expansion; thermal shock; thermal stability; -80 to 80 degC; 1 year; AM0 efficiencies; GaAs-Si; GaAs/Si solar cells; InGaP-InGaAs-Si; MISSE5; Materials International Space Station Experiment number 5; Nomarski optical microscopic examination; SixGe1-x alloys; SixGe1-x-Si; device electrical degradation; electroluminescence image analysis; lattice parameter; metamorphic III-V materials; metamorphic tandem; microcrack density; microcrack formation; microcrack free devices; mismatched structures; on-orbit testing; step graded buffer coating; strain balancing; thermal coefficient of expansion; thermal cycling life testing; thermal shock testing; thermal stability; Conducting materials; Electric shock; Gallium arsenide; III-V semiconductor materials; Life testing; Photovoltaic cells; Thermal conductivity; Thermal degradation; Thermal expansion; Thermal stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Photovoltaic Specialists Conference, 2005. Conference Record of the Thirty-first IEEE
ISSN
0160-8371
Print_ISBN
0-7803-8707-4
Type
conf
DOI
10.1109/PVSC.2005.1488195
Filename
1488195
Link To Document