Publications
Using Nonlinear Zeeman Spectroscopy to obtain In-Situ Magnetic Field Measurement in a Hall Thruster
W. Huang, B. Ngom, and A. Gallimore
A 6-kW Laboratory Hall Thruster with Two Concentric Discharge Channels
R. Liang and A. Gallimore
Mapping the Feasible Design Space of the Nanoparticle Field Extraction Thruster
T. Liu, A. Gallimore, B. Gilchrist, and J. Mirecki-Millunchick
Design of an ECR Gasdynamic Mirror Thruster
R. Tang, A. Gallimore, and T. Kammash
Laser-induced Fluorescence Study of Neutral Xenon Flow Evolution inside a 6-kW Hall Thruster
W. Huang and A. Gallimore
Near-Wall Plasma Properties and EEDF Measurements of a 6-kW Hall Thruster
Rohit Shastry, Alec Gallimore, and Richard Hofer
Laser-Induced Fluorescence of Singly-Charged Xenon Inside a 6-kW Hall Thruster
Wensheng Huang, Brittany Drenkow, and Alec Gallimore
Developing a Reduced Gravity Testbed for the Nanoparticle Field Extraction Thruster
Drenkow, B., Liu, T., Bell, J., Huang, M., Robinson, J., Moore, S., Singh, V., Trabert, R., Gilchrist, B., and Gallimore, A.
Temporally and Spatially Resolved Measurements in the Plume of Clustered Hall Thrusters
Robert Lobbia, Thomas Liu, and Alec Gallimore
Specific Charge Control for Micro/Nano-Particle Electrostatic Propulsion
Thomas Liu, Gregory Wagner, Alec Gallimore, Brian Gilchrist, and Peter Peterson
Operating a radio-frequency plasma source on water vapor
Sonca V. T. Nguyen, John E. Foster, and Alec D. Gallimore
High-speed Planar Plasma Density Measurements in a Hall Thruster Plume
Lobbia, R. B., Liu, T. M., and Gallimore, A. D.
Dissociation of CO2 in a Radio-Frequency Plasma Source
Spencer, L., Gallimore, A., Nguyen, S
Using Crossed Electric and Magnetic Fields to Mitigate Atmospheric Re-Entry Communications Blackout
Lemmer, K. M., and Gallimore, A. D.
Characterization of a Water Radio-Frequency Plasma – An Experimental Study
S. V. T. Nguyen, J. E. Foster, A. D. Gallimore
A Study of Reaction Kinetics of a Water Plasma Using a 0-D Global Kinetic Model
S. V. T. Nguyen, M. J. Kushner, A. D. Gallimore
Micro/Nano-Particle Electrostatic Accelerator for Electric Propulsion
T. M. Liu, A. D. Gallimore, B. E. Gilchrist, P. Y. Peterson
Validating a Plasma Momentum Flux Sensor to an Inverted Pendulum Thrust Stand
Benjamin Longmier, University of Houston; Bryan Reid, University of Michigan; Alec Gallimore, University of Michigan; Franklin Chang-Diaz, Ad Astra Rocket Company; Jared Squire, Ad Astra Rocket Company; Tim Glover, Ad Astra Rocket Company; Greg Chavers, NASA Marshall Space Flight Center; Edgar Bering, University of Houston
Method for analyzing E×B probe spectra from Hall thruster plumes
Rohit Shastry, Richard R. Hofer, Bryan M. Reid, and Alec D. Gallimore
Using a helicon source to simulate atmospheric re-entry plasma densities and temperatures in a laboratory setting
Lemmer, K. M., Gallimore, A. D. and Smith, T. B.
The Nanoparticle Field Extraction Thruster: NanoFET
Massey, D.R., Musinski, L.D., Liu, T.M., Gallimore, A.D., and Gilchrist, B.E.
NanoFET – Nanoparticle Field Extraction Thruster
D. Massey, A. Gallimore, L. Musinski, and T. Liu
Cathode Positioning and Orientation Effects on Cathode Coupling in a 6-kW Hall Thruster
M. McDonald and A. Gallimore
Evaluation of Faraday Probe Design and Scattering Effects on Current Density Measurements of a 200-W Hall Thruster
Brown, D. L., Larson C.W., Nakles, M. R., Gallimore, A. D.