Publications
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.
Low Voltage Characteristics and Cathode Coupling Effects in a 6-kW Hall Thruster
Brown, D. L., Gallimore, A. D.
Correlating Time-Resolved Optical and Langmuir Probe Measurements of Hall Thruster Dynamics
Lobbia, R. B., Liu, T. M., and Gallimore, A. D.
Study of the Synchronous Operation of an Annular Field Reversed Configuration Plasma Device
Kirtley, D. E.
Automating Optimal Interplanetary Trajectories and System Trade Studies
Patel, P. R.
Electrostatic Charging of Micro- and Nano-Particles for Use with Highly Energetic Applications
Musinski, L.D., Liu, T.M., Gilchrist, B.E., and Gallimore, A.D.
Laser-Induced Fluorescence of Singly-Charged Xenon in a 6-kW Hall Thruster Plume
Huang, W., Reid, B. M., Smith, T. B., and Gallimore, A. D.
Plasma Potential Measurements in the Discharge Channel of a 6-kW Hall Thruster
Reid, B. M. and Gallimore, A. D
Statistical Analysis of the Acceleration Zone Location in Hall Thrusters
Linnell, J., and Gallimore, A.D.
Langmuir Probe Measurements in the Discharge Channel of a 6-kW Hall Thruster
Reid, B. M. and Gallimore, A. D.
Reduced Gravity Testing of the Nanoparticle Field Extraction Thruster Concept
Morris, S., Drenkow, B., Liu, T., Biehle, T., Munski, J., Han, H., Swieringa, K., Martinchek, P., Knapp, M., Trabert, R., Wind, R., Brierty, B., Gilchrist, B., and Gallimore, A.
Alpha Particle Dynamics in Muon-Boosted Fusion Propulsion System
Terry Kammash, Ricky Tang, and Alec Gallimore
Nanoparticle Field Extraction Thruster (nanoFET): Introduction to, Analysis of, and Experimental Results from the “No Liquid” Design Option
Musinski, L., Liu, T., Gilchrist, B., and Gallimore, A
Validating a Momentum Flux Sensor with a Hall Thruster Mounted on an Inverted Pendulum Thrust Stand
Longmier, B. W., Reid, B. M., Gallimore, A. D., Chang-Diaz, F. R., Squire, J. P., et al.