1092 Energetics of Propellant Options for High-Power Hall Thrusters
AIAA-2004-6119 Michigan Technological University Aerospace Enterprise
AIAA-2006-1891 Charge Determination for Specified Shape Coulomb Force Virtual Structures
An Efficient Supersonic Wind Tunnel Drive System for Mach 2.5 Flows
An Optical Diagnostic for Xenon Hall Thrusters Including Metastable Contributions
Boundary-Layer Studies In A 2-D Supersonic Nozzle For Quiet-Tunnel Applications
Challenges and Prospects of Coulomb Spacecraft Formations (AAS 03-278)
Coulomb Spacecraft Voltage Study Due to Differential Orbital Perturbations (AAS 06-123)
Design and Testing of Ultralight Fabric Reflux Tubes