DocumentCode
57409
Title
Low-Thrust Geostationary Transfer Orbit (LT2GEO) Radiation Environment and Associated Solar Array Degradation Modeling and Ground Testing
Author
Messenger, Scott R. ; Wong, Francis ; Bao Hoang ; Cress, Cory D. ; Walters, R.J. ; Kluever, Craig A. ; Jones, Glenn
Author_Institution
Univ. of Maryland Baltimore County, Baltimore, MD, USA
Volume
61
Issue
6
fYear
2014
fDate
Dec. 2014
Firstpage
3348
Lastpage
3355
Abstract
Low-thrust geostationary transfer orbits (LT2GEO) are found to offer significant low cost options thus making them very attractive for GEO missions. However, LT2GEOs increase the transfer orbit time from days to months, thereby causing a significant increase in the time that satellites traverse the most intense trapped particle radiation belts. This paper describes the LT2GEO radiation environment and provides some practical implications using new solar cell technologies and materials. New solar cell and coverglass testing protocols are established using Monte Carlo transport modeling and experimental results are given for Qioptiq CMG borosilicate coverglass.
Keywords
Monte Carlo methods; borosilicate glasses; electric propulsion; radiation belts; solar cell arrays; space vehicle power plants; GEO missions; LT2GEO radiation environment; Monte Carlo transport modeling; Qioptiq CMG borosilicate coverglass; associated solar array degradation modeling; coverglass testing protocols; ground testing; low-thrust geostationary transfer orbit; solar cell technologies; transfer orbit time; trapped particle radiation belts; Degradation; Optimization; Orbits; Photovoltaic cells; Protons; Radiation effects; Trajectory; Radiation effects; radiation environments; solar cells;
fLanguage
English
Journal_Title
Nuclear Science, IEEE Transactions on
Publisher
ieee
ISSN
0018-9499
Type
jour
DOI
10.1109/TNS.2014.2364894
Filename
6966817
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