Publications
Internal Plasma Potential Profiles in a Laboratory-Model Hall Thruster
Haas, J.M., and Gallimore, A.D.
The Use of Laser-Induced Fluorescence to Characterize Discharge Cathode Erosion in a 30cm Ring-Cusp Ion Thruster
Williams, G. J.
Mass Spectral Measurements in the Plume of an SPT-100 Hall Thruster
King, L. B., and Gallimore, A. D.
Development of a High-Speed, Reciprocating Electrostatic Probe System for Hall Thruster Interrogation
Haas, J. M., Gallimore, A. D., McFall, K., and Spanjers, G.
Laser-Induced Fluorescence Characterization of Ion Emitted from Hollow Cathodes
Williams, G. J., Smith, T. B., Domonkos, M. T., Gallimore, A. D., and Drake, R. P.
Ion-Energy Diagnostics in the Plasma Exhaust of a Hall Thruster
King, L. B., and Gallimore, A. D.
FMT-2 Discharge Cathode Erosion Rate Measurements via Laser Induced Fluorescence
Williams, G., Smith, T., Gallimore, A.D.
Developing Field Emitter Array Cathode Systems for Electrodynamic Tether Propulsion
Morris, D., Gilchrist, B., Gallimore, A., Jensen, K.
An Investigation of Internal Ion Number Density and Electron Temperature Profiles in a Laboratory-Model Hall Thruster
Haas, J.M., Gallimore, A.D.
Experimental Investigation of Hall Thruster Magnetic Field Topography
Peterson, P.Y., Haas, J.M., Hofer, R.R., Martinez, R.A., and Gallimore, A.D.
Optimization of Hall Thruster Magnetic Field Topography
Hofer, R.R., Haas, J.M., Peterson, P.Y., Martinez, R.A., and Gallimore, A.D.
Spectroscopic Characterization of FMT-2 Discharge Ionization Processes
Smith, T.B., Williams, G.J., Hidaka, Y., Glick, K., and Gallimore, A.D.
Plasma Density Measurements Inside a Laboratory Model Hall Thruster Using a Resonance Probe Diagnostic
Beal, B.E., Haas, J.M., Gallimore, A.D.
Numerical Thermal Model of NASA Solar Electric Propulsion Technology Application Readiness Ion Thruster
Van Noord, J., Gallimore, A. D., and Rawlin, V. K.
Very Near-Field Plume Investigation of the Anode Layer Thruster
Domonkos, M. T., Gallimore, A. D., Marrese, C. M., and Haas, J. M.
Pulse Propagation Along Conductors in Low-density, Cold Plasmas as Applied to Electrodynamic Tethers in the Ionosphere
Bilén, S. G.
Thermal Model of an Ion Thruster
Van Noord, J. L.
Evaluation of Low-Current Orificed Hollow Cathodes
Domonkos, M. T.
Experimental Investigations of Plasma Parameters and Species-Dependent Ion Energy Distribution in the Plasma Exhaust Plume of a Hall Thruster
Kim, S. W.
Examination of the Structure and Evolution of Ion Energy Properties of a 5 kW Class Laboratory Hall Effect Thruster at Various Operational Conditions
Gulczinski, F. S.
Compatibility of Field Emission Cathode and Electric Propulsion Technologies
Marrese, C. M
Characterization of the FMT-2 Discharge Cathode Plume
Williams, G.J., Smith, T.B., Patrick, T.A., and Gallimore, A.D.
Development of a 45-Degree Parallel-Plate Electrostatic Energy Analyzer for Hall Thruster Plume Studies: Preliminary Data
Hofer, R.R., Haas, J.M., and Gallimore, A.D.
Characterization of the Internal Plasma Structure of a 5 kW Hall Thruster
Haas, J.M., and Gallimore, A.D.
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