• DocumentCode
    2788566
  • Title

    Critical analysis of active shielding methods for space radiation protection

  • Author

    Townsend, Lawrence W.

  • Author_Institution
    Dept. of Nucl. Eng., Tennessee Univ., Knoxville, TN, USA
  • fYear
    2005
  • fDate
    5-12 March 2005
  • Firstpage
    724
  • Lastpage
    730
  • Abstract
    From time to time over the past several decades, designs utilizing active methods involving electromagnetic field configurations have been proposed for the purpose of protecting spacecraft crews from harmful space radiations. Designs affording protection from either solar energetic particle event protons or galactic cosmic rays or both have been proposed. Often these analyses are predicated upon simplified or even incorrect assumptions regarding the incident radiation spectra or their associated radiation risks and limits. At times the proponents of these designs make very optimistic assumptions about the abilities of the scientific and engineering communities to overcome existing technology gaps needed to move their designs from paper to practice. In this paper, various active shield methods proposed over the past several decades are reviewed and critiqued. Advantages and disadvantages of the proposed methods are presented. Shortcomings in the analyses of their shielding efficacies, where they exist, are described.
  • Keywords
    aerospace safety; radiation protection; shielding; solar cosmic ray particles; solar radiation; space vehicles; active shielding; electromagnetic field configurations; galactic cosmic rays; radiation risks; solar energetic particle event protons; space radiation protection; spacecraft protection; Cosmic rays; Design engineering; Design methodology; Design optimization; Electromagnetic fields; Electromagnetic radiation; Protection; Protons; Risk analysis; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2005 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-8870-4
  • Type

    conf

  • DOI
    10.1109/AERO.2005.1559364
  • Filename
    1559364