• 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