DocumentCode :
881949
Title :
Spacecraft Fiberglass Strut Charging/Discharging and EMI
Author :
Balmain, K.G. ; Gossland, M. ; Karia, K.
Author_Institution :
Department of Electrical Engineering University of Toronto Toronto, Canada M5S 1A4
Volume :
32
Issue :
6
fYear :
1985
Firstpage :
4438
Lastpage :
4440
Abstract :
Glass-fiber-epoxy struts used in spacecraft extendable masts were exposed to a 20 keV electron beam. Discharges were observed, and near-field measurements used to deduce the radiated emission spectrum for comparison with spacecraft specifications.
Keywords :
Aerospace engineering; Aircraft manufacture; Broadband antennas; Charge measurement; Current density; Current measurement; Electromagnetic interference; Electron beams; Extraterrestrial measurements; Space vehicles;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/TNS.1985.4334138
Filename :
4334138
Link To Document :
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