DocumentCode
2072810
Title
Recent advances in dual-mode Hall effect thruster development
Author
Lazurenko, A. ; Mazouffre, S. ; Prioul, M. ; Duchemin, O. ; Arrat, D. ; Dudeck, M.
Author_Institution
Aerothermique Lab., CNRS, Orleans, France
fYear
2005
fDate
9-11 June 2005
Firstpage
339
Lastpage
343
Abstract
Two SNECMA´s Hall-effect thrusters - the 1.5 kW class PPS®-1350G and the 5 kW class PPS®-X000ML were tested in a wide range of operation parameters. For instance, with a propellant mass-flow rate of 2.3 mg/s for the former and 5 mg/s for the latter, the discharge voltage was ramped up to 1000V. They demonstrated the flexibility in changing of operation parameters and promising performances from the point of view of the dual-mode operation. Particularities about the ion acceleration in the PPS®-X000ML are also presented and discussed in this contribution.
Keywords
Hall effect devices; aerospace engines; ion engines; 1.5 kW; 1000 V; 5 kW; SNECMA; discharge voltage; dual-mode Hall effect thruster development; operation parameters; propellant mass-flow rate; Acceleration; Anodes; Cathodes; Electrons; Hall effect; Laboratories; Propulsion; Space missions; Testing; Voltage;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies, 2005. RAST 2005. Proceedings of 2nd International Conference on
Print_ISBN
0-7803-8977-8
Type
conf
DOI
10.1109/RAST.2005.1512588
Filename
1512588
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