Publications

  • 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

  • The Role of Magnetic Field Topography in Improving the Performance of High-Voltage Hall Thrusters

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

    38th Joint Propulsion Conference, Indianapolis, IN, AIAA-2002-4111, July 7-10, 2002

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

    Walker, M. L. R., Gallimore, A. D., Cai, C., Body, I. D.

    38th Joint Propulsion Conference, Indianapolis, IN, AIAA-2002-3815, July 7-10, 2002

  • Correlating Laser Induced Fluorescence and Molecular Beam Mass Spectrometry Ion Energy Distributions

    Williams, G. J., Smith, T. B., Gulczinski, F. S., Gallimore, A. D.

    Journal of Propulsion and Power, Vol. 18, No. 2, pp. 489-491, March-April 2002

  • Considerations on the Role of the Hall Current in a Laboratory-Model Thruster

    Haas, J. M., and Gallimore, A. D.

    IEEE Transactions on Plasma Science, Vol. 30, No. 2, 687-697, April 2002

  • Current Collection to Long Conductors with Wide Geometries for Bare Electrodynamic Tether Applications: A Laboratory Update

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

    40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA-2002-1123, January 14-17, 2002

  • Low-perturbation Interrogation of the Internal and Near-field Plasma Structure of a Hall Thruster Using a High-Speed Probe Positioning System

    Haas, J. M.

    University of Michigan, Ph.D. Dissertation, 2001

  • Characterizing Vacuum Facility Backpressure Effects on the Performance of a Hall Thruster

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

    27th International Electric Propulsion Conference, Pasadena, CA, IEPC-01-045, October 15-19, 2001

  • A Comparison of Nude and Collimated Faraday Probes for Use with Hall Thrusters

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

    27th International Electric Propulsion Conference, Pasadena, CA, IEPC-01-020, October 15-19, 2001

  • A High Specific Impulse Two-Stage Hall Thruster with Plasma Lens Focusing

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

    27th International Electric Propulsion Conference, Pasadena, CA, IEPC-01-036, October 15-19, 2001

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