Design and operation of hall thruster with segmented electrodes

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Fisch, N J ^a   Raitses, Y ^a   Litvak, A A ^a   Dorf, L A ^a  

^a PRINCETON PLASMA PHYSICS LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTRODES; PROPULSION;

DESIGN AND OPERATIONS; SEGMENTED ELECTRODES; STATE OF THE ART; VACUUM FACILITY;

HALL THRUSTERS;

EID: 77956732209     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Morozov, A. I., “The Study of Plasma Systems with Closed Electron Drift and Distributed Electric Field,” in Plasma Accelerators (ed. L. Artsimovich), Moscow, Mashinostroenie (1973). (in Russian)
2. Fruchtman, A., Fisch, N. J., “Modeling the Hall Thruster,” AIAA 98-3500, Cleveland, Ohio (1998).
3. Brophy, J. R., “Stationary Plasma Thruster Evaluation in Russia,” Jet Propulsion Lab., JPL-92-4, Pasadena, CA (March, 1992).
4. Bugrova, A. I., Kim, V., Maslennikov, N. A., and Morozov, A. I., “Physical Processes and Characteristics of Stationary Plasma Thrusters with Closed Electron Drift,” 22nd Int. Electric Propulsion Conf., IEPC-91-79, Viareggio, Italy (Oct. 1991).
5. Raitses, Y., Ashkenazy, J., “Discharge Characteristics of Hall Current Accelerators,” Proc. XVII Int. Symposium on Discharges and Electrical Insulation in Vacuum, Berkeley, CA (July, 1996).