Publications

  • Evaluation of a Magnetically-Filtered Faraday Probe for measuring the ion current density profile of a Hall thruster

    Rovey, J. L., Walker, M. L. R., Gallimore, A. D., Peterson, P. Y.

    40th Joint Propulsion Conference, Fort Lauderdale, FL, AIAA-2004-3948, July 11-14, 2004

  • The Performance and Plume Characterization of a Laboratory Gridless Ion Thruster with Closed Electron Drift Acceleration

    Peterson, P. Y., Gallimore, A. D.

    40th Joint Propulsion Conference, Fort Lauderdale, FL, AIAA-2004-3936, July 11-14, 2004

  • Discharge Chamber Plasma Structure of a 30-cm NSTAR-type Ion Engine

    Herman, D. A., Gallimore, A. D.

    40th Joint Propulsion Conference, Fort Lauderdale, FL, AIAA-2004-3794, July 11-14, 2004

  • Development of the Top Hat Electric Propulsion Plume Analyzer (TOPAZ)

    Victor, A. L., Zurbuchen, T. H., Gallimore, A. D.

    40th Joint Propulsion Conference, Fort Lauderdale, FL, AIAA-2004-4099, July 11-14, 2004

  • Efficiency Analysis of a High-Specific Impulse Hall Thruster

    Hofer, R. R., Gallimore, A. D.

    40th Joint Propulsion Conference, Fort Lauderdale, FL, AIAA-2004-3602, July 11-14, 2004

  • Near Discharge Cathode Assembly Plasma Potential Measurements in a 30-cm NSTAR-type Ion Engine amidst Beam Extraction

    Herman, D. A., Gallimore, A. D.

    40th Joint Propulsion Conference, Fort Lauderdale, FL, AIAA-2004-3958, July 11-14, 2004

  • Laser-induced Fluorescence Velocimetry of Xe II in the 30-cm NSTAR-type Ion Engine Plume

    Smith, T. B., Herman, D. A., Gallimore, A. D., Williams, G. J.

    40th Joint Propulsion Conference, Fort Lauderdale, FL, AIAA-2004-3963, July 11-14, 2004

  • Deconvolution of Ion Velocity Distributions from Laser-Induced Fluorescence Spectra of Xenon Electrostatic Thruster Plumes

    Smith, T. B

    University of Michigan, Ph.D. Dissertation, 2003

  • Ion Voltage Diagnostics in the Far-Field Plume of a High-Specific Impulse Hall Thruster

    Hofer, R. R., Haas, J. M., Gallimore, A. D.

    39th Joint Propulsion Conference, Huntsville, AL, AIAA-2003-4556, July 20-23, 2003

  • Performance Characteristics of a Cluster of 5 kW Laboratory Hall Thrusters

    Walker, M. L. R., Gallimore, A. D.

    39th Joint Propulsion Conference (JPC), Huntsville, AL, AIAA-2004-3767, July 20-23, 2003

  • Ion Species Fractions in the Far-Field Plume of a High-Specific Impulse Hall Thruster

    Hofer, R. R., Gallimore, A. D.

    39th Joint Propulsion Conference, Huntsville, AL, AIAA-2003-5001, July 20-23, 2003

  • Comparison of Discharge Plasma Parameters in a 30-cm NSTAR Type Ion Engine with and without Beam Extraction

    Herman, D. A., Gallimore, A. D.

    39th Joint Propulsion Conference, Huntsville, AL, AIAA-2003-5162, July 20-23, 2003

  • The Effects of Clustering Multiple Hall Thrusters on Plasma Plume Properties

    Beal, B. E., Gallimore, A. D., Hargus, W. A.

    39th Joint Propulsion Conference, Huntsville, AL, AIAA-2003-5155, July 20-23, 2003

  • Low-Current, Xenon Orificed Hollow Cathode Performance for In-Space Applications

    Domonkos, M. T., Patterson, M. J., and Gallimore, A. D.

    Journal of Propulsion and Power, Vol. 19, No. 3, pp. 438-443, May-June 2003

  • Energy Analysis of a Hall Thruster Cluster

    Beal, B. E., Gallimore, A. D

    28th International Electric Propulsion Conference, Toulouse, France, IEPC-2003-035, March 17-21, 2003

  • Hot Flow Pressure Map of a Vacuum Facility as a Function of Flow Rate to Study Facility Effects

    Walker, M. L. R., Gallimore, A. D.

    28th International Electric Propulsion Conference, Toulouse, France, IEPC-2003-077, March 17-21, 2003

  • Recent Results from Internal and Very-Near-Field Plasma Diagnostics of a High Specific Impulse Hall Thruster

    Hofer, R. R., Gallimore, A. D

    28th International Electric Propulsion Conference, Toulouse, France, IEPC-2003-037, March 17-21, 2003

  • Discharge Plasma Parameters of a 30-cm Ion Thruster Measured without Beam Extraction using a High-Speed Probe Positioning System

    Herman, D. A., McFarlane, D. S., and Gallimore, A. D.

    28th International Electric Propulsion Conference, Toulouse, France, IEPC-2003-069, March 17-21, 2003

  • Plume Study of a 1.35-kW SPT-100 Using an ExB Probe

    Kim, S., and Gallimore, A. D.

    Journal of Spacecraft and Rockets, Vol. 39, No. 6, pp. 904-909, November-December 2002

  • Analysis of chamber simulations of long collecting probes in high-speed dense plasmas

    Gilchrist, B.E., Bilén, S.G., Choiniere, E., Gallimore, A.D., Smith, T.B.

    IEEE Transactions on Plasma Science, Art. No. 01178020 , Volume 30, Issue 5, Part 2, Page(s):2023 - 2034, October 2002

  • An experimental investigation of the internal magnetic field topography of an operating Hall thruster

    Peterson, P. Y., Gallimore, A. D., and Haas, J. M.

    Physics of Plasmas, Vol. 9, No. 10, 4354-4362, Oct. 2002

  • A High-Speed Probe Positioning System for Interrogating the Discharge Plasma of a 30 cm Ion Thruster

    Herman, D. A., Gallimore, A. D.

    38th Joint Propulsion Conference, Indianapolis, IN, AIAA-2002-4256, July 7-10, 2002

  • Preliminary Plume Characterization of a Low-Power Hall Thruster Cluster

    Beal, B. E., Gallimore, A. D., Hargus, W. A.

    38th Joint Propulsion Conference, Indianapolis, IN, AIAA-2002-4251, July 7-10, 2002

  • The Effects of Nude Faraday Probe Design and Vacuum Facility Backpressure on the Measured Ion Current Density Profile of Hall Thruster Plumes

    Walker, M. L. R., Hofer, R. R., Gallimore, A. D

    38th Joint Propulsion Conference, Indianapolis, IN, AIAA-2002-4253, July 7-10, 2002