Plasma Potential Measurements in the Discharge Channel of a 6-kW Hall Thruster

Author:

Reid Bryan,Gallimore Alec

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

1. Haas, J. M., Hofer, R. R., Brown, D. L., Reid, B.M. andGallimore, A. D. "Design of the ##HallThruster forHigh Thrust/Power Investigation,"Presented at the 54th JANNAFPropulsion Meeting,Denver, CO, May14-17,2007.

2. Reid, B. M., Gallimore, A. D., Hofer, R. R., Li, Y. andHaas, J. M. "Anode Designand Verificationfor the ##Hall Thruster,"Presentedat the 54thJANNAF Propulsion Meeting, Denver, CO, May14-17,2007.

3. Hofer, R. R.,Goebel, D.M.andWatkins, R. M."Compact LaB6Hollow Cathodefor the ##HallThruster," Presentedat the54th JANNAF Propulsion Meeting, Denver, CO, May14-17,2007.

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