DocumentCode :
3345151
Title :
Design, analysis & testing of the CellSaver concentrator for spacecraft solar arrays
Author :
Eskenazi, Mike
Author_Institution :
ABLE Eng., Goleta, CA, USA
fYear :
2002
fDate :
19-24 May 2002
Firstpage :
935
Lastpage :
938
Abstract :
CellSaver is an on-panel reflective concentrator used to significantly reduce the cost of spacecraft multijunction solar cell arrays. CellSaver is a unique concentrator because it can easily be retrofit on to existing solar array platforms due to its compatibility with standard large area multi-junction solar cells and standard composite solar panels and its ability to stow in very small panel gaps (<1 cm.) This paper presents CellSaver design details and space flight qualification test results. Detailed test data is given for electrical performance measurements with EMCORE and Spectrolab triple-junction cell strings, GEO thermal cycling, stowed random vibration, and electron, proton and UV radiation exposure.
Keywords :
artificial satellites; electron beam effects; proton effects; semiconductor device measurement; solar cell arrays; ultraviolet radiation effects; CellSaver concentrator; GEO thermal cycling; UV radiation exposure; electrical performance measurements; electron radiation exposure; large area multi-junction solar cells; proton radiation exposure; space flight qualification test results; spacecraft solar arrays; stowed random vibration; Aerospace engineering; Coatings; Costs; Photovoltaic cells; Qualifications; Reflectivity; Silver; Space vehicles; Testing; Titanium;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Photovoltaic Specialists Conference, 2002. Conference Record of the Twenty-Ninth IEEE
ISSN :
1060-8371
Print_ISBN :
0-7803-7471-1
Type :
conf
DOI :
10.1109/PVSC.2002.1190734
Filename :
1190734
Link To Document :
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