Publications

  • Erosion Characterization via Ion Power Deposition Measurements in a 6-kW Hall Thruster

    R. Shastry, A. D. Gallimore, and R. R. Hofer

    57th Joint Army Navy NASA Air Force (JANNAF) Propulsion Meeting, Colorado Springs, CO, May 3-7, 2010

  • Development of a 3D Electron Trajectory Model with Monte Carlo Neutral Collisions for the Hall Thruster Near-Field Plume

    M. S. McDonald, A. D. Gallimore, R. R. Hofer, and D. M. Goebel

    57 th Joint Army Navy NASA Air Force (JANNAF) Propulsion Meeting, Colorado Springs, CO, May 3-7, 2010

  • Development of Real-Time Boron Nitride Erosion Monitoring System for Hall Thrusters by Cavity Ring-Down Spectroscopy

    Yamamoto, N. Y., Yalin, A. P., Tao, L, Smith, T. B., Gallimore, A. D., and Arakawa, Y.

    Trans. JSASS Science Tech. Japan, doi: 10.2322/tstj.7.Pb_1 , vol. 7, no. ists26 Pb_1-Pb_6, 2009

  • Experimental Results for Communications Blackout Amelioration Using Crossed Electric and Magnetic Fields

    Kristina Lemmer, Alec Gallimore,Timothy Smith, Christopher Davis, and Peter Peterson

    Journal of Spacecraft and Rockets, doi: 10.2514/1.45490 , 0022-4650 vol. 46, no. 6 (1100-1109), November-December 2009

  • The Influence of Neutral Flow Rate in the Operation of Hall Thrusters

    Reid, B. M.

    University of Michigan, Ph.D. Dissertation, 2009

  • Hydrogen Production in a Radio-Frequency Plasma Source Operating on Water Vapor

    Nguyen, S. V. T.

    University of Michigan, Ph.D. Dissertation, 2009

  • Methodology and Historical Perspective of a Hall Thruster Efficiency Analysis

    Daniel Brown, C. Larson, Brian Beal, and Alec Gallimore

    Journal of Propulsion and Power, doi: 10.2514/1.38092 , 0748-4658 vol. 25, no. 6 (1163-1177), November-December 2009

  • Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System

    Lemmer, K. M.

    University of Michigan, Ph.D. Dissertation, 2009

  • Magnetic Field Simulation and Mapping Based on Zeeman-split Laser-induced Fluorescence Spectra of Xenon in the Discharge Channel of 5-6 kW Coaxial Stationary-Plasma Hall Thrusters

    Ngom, B. B

    University of Michigan, Ph.D. Dissertation, 2009

  • Investigation of Low Discharge Voltage Hall Thruster Characteristics and Evaluation of Loss Mechanisms

    Brown, D. L.

    University of Michigan, Ph.D. Dissertation, 2009

  • Near-field Ion Current Density Measurements of a 6-kW Hall Thruster

    B. Reid and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-124, September 20-24, 2009

  • An Algorithm for Generating Feasible Low Thrust Interplanetary Trajectories

    P. Patel, A. Gallimore, D. Scheeres, and T. Zurbuchen

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-219, September 20-24, 2009

  • Investigation of Low Discharge Voltage Hall Thruster Operating Modes and Ionization Processes

    D. Brown and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-074, September 20-24, 2009

  • Hall Thruster Electron Motion Characterization Based on Internal Probe Measurements

    J. Linnell and A. Gallimore

    31stInternational Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-105, September 20-24, 2009

  • Cathode Coupling Response to Cathode Placement and Orientation in a 6-kW Hall Thruster

    M. McDonald and A. Gallimore

    31stInternational Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-113, September 20-24, 2009

  • High-Speed Interrogation of the Near-Field Plume of a 6-kW Laboratory Hall Thruster

    M. McDonald and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-112, September 20-24, 2009

  • Using a Helicon Source to Simulate Atmospheric Re-entry Plasma Densities,”

    K. Lemmer and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-236, September 20-24, 2009

  • Evaluation of Plume Divergence and Facility Effects on Far-Field Faraday Probe Current Density Profiles

    D. Brown and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, USA, IEPC-2009-030, September 20-24, 2009

  • Near-Wall Plasma Characterization of a 6-kW Hall Thruster

    R. Shastry, A. Gallimore, and Richard R. Hofer

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-133, September 20-24, 2009

  • A Device for Studying Plasma Detachment from a Magnetic Field

    A. Shabshelowitz and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, September 20-24, 2009

  • Two-dimensional Time-resolved Breathing Mode Plasma Fluctuation Variation with Hall Thruster Discharge Settings

    R. Lobbia and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-106, September 20-24, 2009

  • Using Nonlinear Zeeman Spectroscopy to obtain In-Situ Magnetic Field Measurement in a Hall Thruster

    W. Huang, B. Ngom, and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-088, September 20-24, 2009

  • A 6-kW Laboratory Hall Thruster with Two Concentric Discharge Channels

    R. Liang and A. Gallimore

    31st International Electric Propulsion Conference, Ann Arbor, MI, September 20-24, 2009

  • Mapping the Feasible Design Space of the Nanoparticle Field Extraction Thruster

    T. Liu, A. Gallimore, B. Gilchrist, and J. Mirecki-Millunchick

    31st International Electric Propulsion Conference, Ann Arbor, MI, IEPC-2009-004, September 20-24, 2009