• DocumentCode
    1766251
  • Title

    Azimuthal Spoke Propagation in Hall Effect Thrusters

  • Author

    Sekerak, Michael J. ; Longmier, Benjamin W. ; Gallimore, Alec D. ; Brown, Daniel L. ; Hofer, Richard R. ; Polk, James E.

  • Author_Institution
    Dept. of Aerosp. EngineeringPlasmadynamics, Univ. of Michigan, Ann Arbor, MI, USA
  • Volume
    43
  • Issue
    1
  • fYear
    2015
  • fDate
    Jan. 2015
  • Firstpage
    72
  • Lastpage
    85
  • Abstract
    Spokes are azimuthally propagating perturbations in the plasma discharge of Hall effect thrusters (HETs) that travel in the E x B direction. The mechanisms for spoke formation are unknown, but their presence has been associated with improved thruster performance in some thrusters motivating a detailed investigation. The propagation of azimuthal spokes are investigated in a 6 kW HET by using high-speed imaging and azimuthally spaced probes. The spoke velocity is determined from high-speed image analysis using three methods with similar results. The spoke velocity for three discharge voltages (300, 400, and 450 V) and three anode mass flow rates (14.7, 19.5, and 25.2 mg/s) are between 1500 and 2200 m/s across a range of magnetic field settings. The spoke velocity is inversely dependent on magnetic field strength for lower B-fields and asymptotes at higher B-fields. Spoke velocities calculated from the probes are consistently higher by 30% or more. An empirically approximated dispersion relation of ωα = vchαkθα - ωchα where α ≥ 1 yields a characteristic velocity that matches the ion acoustic speed for N5 eV electrons which exist in the near-anode and near-field plume regions of the discharge.
  • Keywords
    discharges (electric); ion engines; plasma devices; plasma ion acoustic waves; plasma magnetohydrodynamics; plasma probes; Hall effect thrusters; anode mass flow rates; azimuthally propagating perturbation; azimuthally spaced probes; dispersion relation; high-speed image analysis; ion acoustic speed; magnetic field strength; plasma discharge; plasma probes; power 6 kW; spoke velocity; velocity 1500 m/s to 2200 m/s; voltage 300 V; voltage 400 V; voltage 500 V; Discharges (electric); Magnetic resonance imaging; Magnetic separation; Magnetoacoustic effects; Oscillators; Plasmas; Probes; Aerospace industry; hall effect devices; plasma diagnostics; plasma measurements; plasma waves; satellites; space technology; space technology.;
  • fLanguage
    English
  • Journal_Title
    Plasma Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0093-3813
  • Type

    jour

  • DOI
    10.1109/TPS.2014.2355223
  • Filename
    6919317