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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
An Efficient Supersonic Wind Tunnel Drive System for Mach 2.5 Flows
Energy Efficiency in Low Voltage Hall Thrusters AIAA Paper
An Optical Diagnostic for Xenon Hall Thrusters Including Metastable Contributions
Performance Characteristics for a Low I sp Hall Thruster
Mobility Studies of a Pure Electron Plasma in Hall Thruster Fields
AIAA-2006-1891 Charge Determination for Specified Shape Coulomb Force Virtual Structures
Performance Characteristics of a LaB6 Bismuth Cathode for use with Hall Thrusters
Magnesium Hall Thruster with Active Thermal Mass Flow Control
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