• DocumentCode
    1936020
  • Title

    Geometric optimization for radiation hardness assurance

  • Author

    Northum, J. ; Guetersloh, S.

  • Author_Institution
    Dept. of Nucl. Eng., Texas A&M Univ., College Station, TX, USA
  • fYear
    2013
  • fDate
    2-9 March 2013
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    The probability of a single event effect occurring is generally a function of the energy deposited in a sensitive volume, which is typically expressed as the absorbed dose in that volume. For short segments of high energy particle tracks, the dose due to a single event is proportional to the chord length through the sensitive volume. Thus, the distribution of dose in chord length is likely to relate to the probability of single event effects. For various geometries, a differential chord length distribution was generated and from this the dose distribution, frequency mean chord length, and dose mean chord length were calculated. In every case, the dose mean chord length was greater than the frequency mean chord length by a minimum of 26% and increased with the eccentricity of the volume. The large value of the dose mean chord length relative to the frequency mean chord length demonstrates the need to consider rare, long-chord-length crossings in radiation hardness testing, despite their relatively low probability of occurrence.
  • Keywords
    dosimetry; radiation hardening (electronics); statistical distributions; differential chord length distribution; dose distribution; dose mean chord length; frequency mean chord length; geometric optimization; high energy particle track; long chord length crossing; radiation hardness assurance; radiation hardness testing; single event effect; Educational institutions; Electronic components; Geometry; Ionizing radiation; Microelectronics; Shape; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2013 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4673-1812-9
  • Type

    conf

  • DOI
    10.1109/AERO.2013.6496963
  • Filename
    6496963