• DocumentCode
    1455527
  • Title

    Shielding electronics behind composite structures

  • Author

    Spieth, B.D. ; Qassim, K.S. ; Pittman, R.N. ; Russell, D.A.

  • Author_Institution
    ITN Energy Syst., Wheat Ridge, CO, USA
  • Volume
    45
  • Issue
    6
  • fYear
    1998
  • fDate
    12/1/1998 12:00:00 AM
  • Firstpage
    2752
  • Lastpage
    2757
  • Abstract
    The increasing use of composite structures and composite electronics boxes in space can result in a several-fold increase in electronics radiation total dose, as compared to using aluminum structures and aluminum electronics boxes. There are also desires to use multi-function structures (MFS), where electronics are integral with composite structures (no electronics boxes). MFS approaches can result in an order of magnitude increase in radiation dose to electronics over conventional aluminum structures and boxes. The designer must either use rad-hard parts which are becoming more difficult to obtain since the end of the Cold War, increase spot shielding, use RADPAKTM solutions, or add shielding to composite boxes and structures. With the increasing use of low hardness commercial parts to reduce costs, a brute force solution of adding shielding to composite boxes is frequently the lowest cost solution. Analyses, test data, and a flight experiment are described to assess these shielding options
  • Keywords
    aerospace testing; packaging; shielding; space vehicle electronics; RADPAK; composite electronics boxes; composite structures; flight experiment; multi-function structures; rad-hard parts; radiation total dose; space vehicle electronics; spot shielding; Aerospace electronics; Aluminum; Belts; Costs; Geometry; Laboratories; Low earth orbit satellites; Radiation hardening; Space heating; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Nuclear Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9499
  • Type

    jour

  • DOI
    10.1109/23.736524
  • Filename
    736524