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Operating the Helicon Double Layer Thruster in a Space Simulation Chamber.

Authors :
Charles, Christine
Boswell, Rod
Alexander, Peter
Costa, Costanzo
Sutherland, Orson
Pfitzner, Leigh
Franzen, Roger
Kingwell, Jeff
Parfitt, Andrew
Frigot, Pierre-Etienne
Del Amo, Jose
Saccoccia, Georgio
Source :
IEEE Transactions on Plasma Science. Aug2008 Part 1 of 5, Vol. 36 Issue 4, p1196-1197. 2p. 1 Black and White Photograph, 1 Diagram.
Publication Year :
2008

Abstract

A prototype of the helicon double layer thruster (HDLT) is designed and manufactured. Initial tests with the thruster mounted on a small vacuum chamber (pumping speed of 700 l · s-1) show successful operation in xenon with the formation of the double layer which generates a low divergence ion beam, which is the source of thrust. The prototype is subsequently inserted inside a much larger space simulation chamber (pumping speed of 7000 l · s-1). A high-density blue mode is found when increasing the RF power above 380 W, and measurements with a Langmuir probe give an estimated density of 1012 cm-3 in the thruster. An image of the HDLT operating in the high-density blue mode is presented. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
00933813
Volume :
36
Issue :
4
Database :
Academic Search Index
Journal :
IEEE Transactions on Plasma Science
Publication Type :
Academic Journal
Accession number :
34217123
Full Text :
https://doi.org/10.1109/TPS.2008.924425