Spacecraft Fiberglass Strut Charging/Discharging and EMI
Balmain, K. G.
Gossland, M.
Karia, K.
Department of Electrical Engineering University of Toronto Toronto, Canada M5S 1A4;
This paper appears in: Nuclear Science, IEEE Transactions on
Publication Date: Dec. 1985
Volume: 32,
Issue: 6
On page(s): 4438-4440
Location: Snowmass Village, CO, USA,
ISSN: 0018-9499
Digital Object Identifier: 10.1109/TNS.1985.4334138
Current Version Published: 2007-11-12
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.
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