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
Link To Document :
بازگشت