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
Link To Document :
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