DocumentCode
888733
Title
The effects of 1 kW class arcjet thruster plumes on spacecraft charging and spacecraft thermal control materials
Author
Bogorad, A. ; Lichtin, D.A. ; Bowman, C. ; Armenti, J. ; Pencil, E. ; Sarmiento, C.
Author_Institution
General Electric Co., Princeton, NJ, USA
Volume
39
Issue
6
fYear
1992
fDate
12/1/1992 12:00:00 AM
Firstpage
1783
Lastpage
1789
Abstract
Arcjet thrusters are soon to be used for north/south stationkeeping on commercial communications satellites. A series of tests was performed to evaluate the possible effects of these thrusters on spacecraft charging and the degradation of thermal control material. During the tests the interaction between arcjet plumes and both charged and uncharged surfaces did not cause any significant material degradation. In addition, firing an arcjet thruster benignly reduced the potential of charged surfaces to near zero
Keywords
aerospace propulsion; electric propulsion; spacecraft charging; thermal insulation; 1 kW; arcjet thruster plumes; commercial communications satellites; north/south stationkeeping; spacecraft charging; thermal control materials; Aircraft manufacture; Electrostatic discharge; Electrostatic interference; Firing; Propulsion; Space vehicles; Surface charging; Surface contamination; Surface discharges; Thermal pollution;
fLanguage
English
Journal_Title
Nuclear Science, IEEE Transactions on
Publisher
ieee
ISSN
0018-9499
Type
jour
DOI
10.1109/23.211367
Filename
211367
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