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Operating the Helicon Double Layer Thruster in a Space Simulation Chamber.
- 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]
- Subjects :
- *PLASMA devices
*XENON
*ION bombardment
*PLASMA density
*VACUUM
Subjects
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