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
Link To Document :
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