Background Pressure Effects on Ion Velocity Distribution Within a Medium-Power Hall Thruster

5 torr). In addition to varying the background pressure, the radial magnetic field of the thruster was varied (by a factor of 2) between low- and high-strength configurations. The low- strength configuration produced large-magnitude anode current oscillations, whereas the high-strength configuration produced small current oscillations. Ion axial velocity distribution function peaks were used to approximate ion energy and, in turn, axial electric field strength. Acceleration profiles of the tested thruster operatingconditionswerecompared.Highbackgroundpressureoperationwasobservedtoshifttheionacceleration regionupstreaminthedischargechannel. Thewidthofthevelocitydistributionscorrelatedstrongly tothemagnetic field strength. The high magnetic field strength configuration produced narrow velocity distribution functions, whereas the low magnetic field strength configuration led to a broad velocity distribution.

[1]  J. Bearden,et al.  Atomic energy levels , 1965 .

[2]  R. Summers Empirical Observations on the Sensitivity of Hot Cathode Ionization Type Vacuum Gages , 1969 .

[3]  R. Bengtson,et al.  Transition Probabilities of Xe I and Xe II , 1973 .

[4]  H. Schäfer,et al.  Isotope shifts in the atomic spectrum of xenon and nuclear deformation effects , 1974 .

[5]  W. Persson,et al.  Revised analysis of singly ionized xenon, Xe II , 1987 .

[6]  D. Neuschäfer,et al.  Hyperfine splitting measurements on the 6265 Å and 6507 Å lines of seven Xe isotopes by LIF on a beam of metastable Xe(3P0,2) atoms , 1988 .

[7]  D. Manzella Stationary Plasma Thruster Ion Velocity Distribution , 1994 .

[8]  J. Lidberg,et al.  HYPERFINE-STRUCTURE MEASUREMENTS IN XE II , 1996 .

[9]  E. Choueiri Plasma oscillations in Hall thrusters , 2001 .

[10]  M. Cappelli,et al.  Laser-induced fluorescence measurements of velocity within a Hall discharge , 2001 .

[11]  François Rogier,et al.  Determination of the ionization and acceleration zones in a stationary plasma thruster by optical spectroscopy study: Experiments and model , 2001 .

[12]  Alec D. Gallimore,et al.  Characterizing Vacuum Facility Backpressure Effects on the Performance of a Hall Thruster , 2001 .

[13]  Alec D. Gallimore,et al.  Effect of Backpressure on Ion Current Density Measurements in Hall Thruster Plumes , 2005 .

[14]  Evolution of the Ion Velocity Distribtuion in the Near Field of the BHT-200-X3 Hall Thruster , 2006 .

[15]  Alec D. Gallimore,et al.  Performance characteristics of a cluster of 5-kW laboratory hall thrusters , 2007 .

[16]  W. Hargus,et al.  Ion Velocity Measurements Within the Acceleration Channel of a Low-Power Hall Thruster , 2008, IEEE Transactions on Plasma Science.

[17]  S. Mazouffre Laser-induced fluorescence diagnostics of the cross-field discharge of Hall thrusters , 2012 .