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