DocumentCode
2738405
Title
IMM experimentation in the next frontier: Emcore´S participation in the MISSE-8 program
Author
Cho, Benjamin ; Lutz, R. ; Pappan, J. ; Downard, E. ; Cornfeld, A. ; Fatemi, N. ; Stan, M.A. ; Sharps, P. ; Su, C. ; Billets, S. ; Gasner, S. ; Howard, Alex
Author_Institution
Emcore Photovoltaics, Albuquerque, NM, USA
fYear
2010
fDate
20-25 June 2010
Abstract
In collaborations with both Lockheed-Martin (LM) and the Air Force Research Laboratory (AFRL), Emcore has incorporated its cutting-edge IMM cell technologies on MISSE-8 in a variety of cell form factors and two distinct configurations. The first is a double coverglass (DCG) arrangement, where adhesive and coverglass are attached to both the front and backsides of the solar cell, and in the second configuration the IMM cell was mounted to a rigid, lightweight, CTE-matched substrate. Pre-build test coupons were subjected to 1124 thermal cycles from -100 to 100°C, and showed no electrical degradation in six out of seven cells/strings, with the lone degraded cell exhibiting just a 3.5% loss in Jsc and no change in Voc or FF. The average AM0 efficiency (solar constant = 1353 W/m2) of the IMM3J cells flown in this experiment have an average efficiency of 31.3% (omitting an anomalously low-perfoming cell), and the 4cm2 IMM4J cells 33.1%.
Keywords
solar cells; Air Force Research Laboratory; CTE matched substrate; Lockheed-Martin; double coverglass arrangement; solar cell; temperature -100 degC to 100 degC; Computer architecture; Degradation; Microprocessors; Photovoltaic cells; Substrates; Testing; Thermal degradation;
fLanguage
English
Publisher
ieee
Conference_Titel
Photovoltaic Specialists Conference (PVSC), 2010 35th IEEE
Conference_Location
Honolulu, HI
ISSN
0160-8371
Print_ISBN
978-1-4244-5890-5
Type
conf
DOI
10.1109/PVSC.2010.5614513
Filename
5614513
Link To Document