Publications
Top hat electrostatic analyzer for far-field electric propulsion plume diagnostics
Victor, A.L., Zurbuchen, T.H., and Gallimore, A.D.
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.
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.
Plasma properties downstream of a low-power Hall thruster
Beal, B.E., Gallimore, A.D., and Hargus, W.A.
Effects of Facility Backpressure on the Performance and Plume of a Hall Thruster
Walker, M. L. R
A Field Reversed Configuration Plasma Device for Space Propulsion
D. Kirtley, J. M. Haas, A. Gallimore
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.
Potential Structure and Propellant Flow Rate Theory for Ion Thruster Discharge Cathode Erosion
Rovey, J. L., Herman, D. A., Gallimore, A. D.
Scalable Flat-Panel Nano-Particle MEMS/NEMS Thruster
Musinski, L., Liu, T., Gilchrist, B., Gallimore, A. D., and Keidar, M.
Internal Plasma Structure Measurements of a Hall Thruster Using Xenon and Krypton Propellant
Linnell, J. A., Gallimore, A. D
Details on an Annular Field Reversed Configuration Plasma Device for Spacecraft Propulsion
Kirtley, D., Brown, D., Gallimore, A. D.
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.
Evaluation and Active Control of Clustered Hall Thruster Discharge Oscillations
Lobbia, R.B., Gallimore, A.D.
Internal Plasma Structure Measurements of a Hall Thruster Using Plasma Lens Focusing
Linnell, J.A., Gallimore, A.D
Efficiency Analysis of a Hall Thruster Operating with Krypton and Xenon
Linnell, J.A., Gallimore, A.D.
Discharge Cathode Electron Energy Distribution Functions in a 40-cm NEXT-type Ion Engine
Herman, D. A., Gallimore, A. D.
The Effects of Cathode Configuration on Hall Thruster Cluster Plume Properties
Beal, B.E., Gallimore, A.D., and Hargus, Jr., W.A
Discharge Chamber Plasma Potential Mapping of a 40-cm NEXT-type Ion Engine
Herman, D. A., Gallimore, A. D.
The Top Hat Electric Propulsion Plume Analyzer (TOPAZ): Preliminary Data on the BHT600 Cluster
Victor, A. L., Zurbuchen, T. H., Gallimore, A. D
Discharge Chamber Plasma Structure of a 40-cm NEXT-type Ion Engine
Herman, D. A., Gallimore, A. D
Diode Laser-Induced Fluorescence of Xenon Ion Velocity Distributions
Smith, T.B., Ngom, B.B., Linnell, J.A., Gallimore, A.D.
Dormant Cathode Plasma Properties and Erosion Analysis in a Multiple-Cathode, High-Power, Rectangular Discharge Chamber
Rovey, J.L., Gallimore, A.D
Design and Operation of a Multiple-Cathode, High-Power, Rectangular Discharge Chamber
Rovey, J.L., Gallimore, A.D.
Effect of Backpressure on Ion Current Density Measurements in Hall Thruster Plumes
Walker, M.L.R., Victor, A.L., Hofer, R.R., and Gallimore, A.D.
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