A time-resolved laser induced fluorescence study on the ion velocity distribution function in a Hall thruster after a fast current disruption Phys. Plasmas 16, 043504 (2009); 10.1063/1.3112704 Internal plasma potential measurements of a Hall thruster using xenon and krypton propellant Phys. Plasmas 13, 093502 (2006); 10.1063/1.2335820 Spectral analysis of Hall-effect thruster plasma oscillations based on the empirical mode decompositionPlasma oscillations from 0-100 kHz in a 6-kW magnetically shielded Hall thruster are experimentally characterized with a high-speed, optical camera. Two modes are identified at 7-12 kHz and 70-90 kHz. The low frequency mode is found to be azimuthally uniform across the thruster face, while the high frequency oscillation is peaked close to the centerline-mounted cathode with an m ¼ 1 azimuthal dependence. An analysis of these results in the context of wavebased theory suggests that the low frequency wave is the breathing mode oscillation, while the higher frequency mode is gradient-driven. The effect of these oscillations on thruster operation is examined through an analysis of thruster discharge current and a comparison with published observations from an unshielded variant of the thruster. Most notably, it is found that although the oscillation spectra of the two thrusters are different, they exhibit nearly identical steady-state behavior. V C 2014 AIP Publishing LLC. [http://dx.doi.org/10.1063/1.4879819] PHYSICS OF PLASMAS 21, 053512 (2014) This article is copyrighted as indicated in the article. Reuse of AIP content is subject to the terms at: http://scitation.aip.org/termsconditions. Downloaded to IP: 193.0.65.67 On: Tue, 25 Nov 2014 14:28:57 FIG. 3. (a) Phase of the mode at 7-12 kHz as a function of normalized position. The reference point ðr 0 ; h 0 Þ employed to generate this plot is located in the channel. (b) Phase of the mode at 70-90 kHz. The reference point ðr 0 ; h 0 Þ for this plot is located off-axis at r 0 ¼ 0.05r c .