Publications

  • The Student Space Systems Fabrication Laboratory: An Approach to Space Systems Engineering Education

    Liu, T., Deline, C., Ramos, R., Sandoval, S., Smetana, A., Gilchrist, B., Washabaugh, P., and Renno, N

    113th ASEE Conference, Chicago, IL, 18-21 June 2006

  • Development, Fabrication and Testing of a 15-cm-diameter Helicon Source

    Lemmer, K. M., Gallimore, A. D., Morris, D. P., Davis, C., Boyd, I., and Keidar, M

    33rd IEEE International Conference on Plasma Science (ICOPS) Traverse City, MI, June 4-8, 2006

  • Breakdown and Ignition Limits in LaB6 Hollow Cathode Discharges

    Tang, R., Nguyen, S., Smith, T.B., and Gallimore, A.D.

    33rd IEEE International Conference on Plasma Science (ICOPS) Traverse City, MI, ICOPS Presentation, June 4-8, 2006

  • Optogalvanic spectroscopy of the Zeeman effect in xenon

    Smith, T.B., Ngom, B., and Gallimore, A.D.

    33rd IEEE International Conference on Plasma Science (ICOPS) Traverse City, MI, ICOPS Presentation, June 4-8, 2006

  • Ion Collection in Hall Thruster Plumes

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

    Journal of Propulsion and Power, 0748-4658 vol.22 no.1 (205-209), January-February 2006

  • Top hat electrostatic analyzer for far-field electric propulsion plume diagnostics

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

    Review of Scientific Instruments, Art. No. 013505 , Volume 77, January 2006

  • 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., and Peterson, P.Y.

    Review of Scientific Instruments, Art. No. 013503 , Volume 77, January 2006

  • The Use of Electrostatic Probes to Characterize the Discharge Plasma Structure and Identify Discharge Cathode Erosion Mechanisms in Ring-Cusp Ion Thrusters

    Herman, D. A.

    University of Michigan, Ph.D. Dissertation, 2005

  • Plasma properties downstream of a low-power Hall thruster

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

    Physics of Plasmas, Art. No. 123503 , Vol. 12, Issue 12, December 2005

  • Effects of Facility Backpressure on the Performance and Plume of a Hall Thruster

    Walker, M. L. R

    University of Michigan, Ph.D. Dissertation, 2005

  • A Field Reversed Configuration Plasma Device for Space Propulsion

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

    29th International Electric Propulsion Conference (IEPC), Princeton, NJ, Oct 31-Nov 4, 2005

  • Development of the Top Hat Electric Propulsion Plume Analyzer (TOPAZ): Mass Analyzer Design and Preliminary Calibration Data

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

    29th International Electric Propulsion Conference, Princeton, NJ, IEPC-2005-016, Oct 31-Nov 4, 2005

  • Potential Structure and Propellant Flow Rate Theory for Ion Thruster Discharge Cathode Erosion

    Rovey, J. L., Herman, D. A., Gallimore, A. D.

    29th International Electric Propulsion Conference, Princeton, NJ, IEPC-2005-022, Oct 31-Nov 4, 2005

  • Scalable Flat-Panel Nano-Particle MEMS/NEMS Thruster

    Musinski, L., Liu, T., Gilchrist, B., Gallimore, A. D., and Keidar, M.

    29th International Electric Propulsion Conference, Princeton, NJ, IEPC-2005-176, Oct 31-Nov 4, 2005

  • Internal Plasma Structure Measurements of a Hall Thruster Using Xenon and Krypton Propellant

    Linnell, J. A., Gallimore, A. D

    29th International Electric Propulsion Conference, Princeton, NJ, IEPC-2005-024, Oct 31- Nov 4, 2005

  • Details on an Annular Field Reversed Configuration Plasma Device for Spacecraft Propulsion

    Kirtley, D., Brown, D., Gallimore, A. D.

    29th International Electric Propulsion Conference, Princeton, NJ, IEPC-2005-171, Oct 31- Nov 4, 2005

  • Experimental Investigation of Electron Collection to Solid and Slotted Tape Probes in a High-Speed Flowing Plasma

    Choiniere, E., Bilén, S.G., Gilchrist, B.E., Fuhrhop, K.R., Gallimore, A.D.

    IEEE Transactions on Plasma Science, Art. No. 01495579 , Volume 33, Issue 4, Part 2, Page(s):1310 - 1323, August 2005

  • Evaluation and Active Control of Clustered Hall Thruster Discharge Oscillations

    Lobbia, R.B., Gallimore, A.D.

    41st Joint Propulsion Conference, Tucson, AZ, AIAA-2005-3679, July 10-13, 2005

  • Internal Plasma Structure Measurements of a Hall Thruster Using Plasma Lens Focusing

    Linnell, J.A., Gallimore, A.D

    41st Joint Propulsion Conference, Tucson, AZ, AIAA-2005-4402, July 10-13, 2005

  • Efficiency Analysis of a Hall Thruster Operating with Krypton and Xenon

    Linnell, J.A., Gallimore, A.D.

    41st Joint Propulsion Conference, Tucson, AZ, AIAA-2005-3683, July 10-13, 2005

  • Discharge Cathode Electron Energy Distribution Functions in a 40-cm NEXT-type Ion Engine

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

    41st Joint Propulsion Conference, Tucson, AZ, AIAA-2005-4252, July 10-13, 2005

  • The Effects of Cathode Configuration on Hall Thruster Cluster Plume Properties

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

    41st Joint Propulsion Conference, Tucson, AZ, AIAA-2005-3678, July 10-13, 2005

  • Discharge Chamber Plasma Potential Mapping of a 40-cm NEXT-type Ion Engine

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

    41st Joint Propulsion Conference, Tucson, AZ, AIAA-2005-4251, July 10-13, 2005

  • The Top Hat Electric Propulsion Plume Analyzer (TOPAZ): Preliminary Data on the BHT600 Cluster

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

    41st Joint Propulsion Conference, Tucson, AZ, AIAA-2005-3870, July 10-13, 2005