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AIAA-2004-6119 Michigan Technological University Aerospace Enterprise
1092 Energetics of Propellant Options for High-Power Hall Thrusters
Re-Generable Field Emission Cathodes for Low-Power Electric Propulsion AIAA Paper
Energy Efficiency in Low Voltage Hall Thrusters AIAA Paper
An Efficient Supersonic Wind Tunnel Drive System for Mach 2.5 Flows
An Optical Diagnostic for Xenon Hall Thrusters Including Metastable Contributions
Mobility Studies of a Pure Electron Plasma in Hall Thruster Fields
Performance Characteristics for a Low I sp Hall Thruster
AIAA-2006-1891 Charge Determination for Specified Shape Coulomb Force Virtual Structures
Performance Characteristics of a LaB6 Bismuth Cathode for use with Hall Thrusters
Flow Characteristics of the NASA-Ames Laminar Flow Supersonic Wind Tunnel for Mach 1.6 Operation
Boundary-Layer Studies In A 2-D Supersonic Nozzle For Quiet-Tunnel Applications
Coulomb Spacecraft Voltage Study Due to Differential Orbital Perturbations (AAS 06-123)
Challenges and Prospects of Coulomb Spacecraft Formations (AAS 03-278)
HYDRODYNAMIC ASPECTS OF A FAST CATAMARAN OPERATING IN SHALLOW WATER