• 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