High-Current Lanthanum Hexaboride Hollow Cathode for High-Power Hall Thrusters
AIAA-2004-5911 Extending Hollow Cathode Life for Electric Propulsion for Long-Term Missions
Analytical Discharge Performance Model for rf and Kaufman Ion Thrusters AIAA Paper
Ion Thruster Discharge Performance per Magnetic Field Topography
Performance Evaluation of an Expanded Range XIPS Ion Thruster System for NASA Science Missions
Alternative Kraftstoffe im Verkehr: Die Bedeutung von Erdgas in der zukuenftigen Mobilitaet
Neutral Density Measurements in a Hall Thruster Plume AIAA Paper
Neutral Density Measurements in an NSTAR Ion Thruster
Low Current Cerium Hexaboride and Lanthanum Hexaboride Hollow Cathodes
Wall Sheath and Electron Mobility Modeling in Hybrid-PIC Hall Thruster Simulations AIAA Paper
Effects of an Internally-Mounted Cathode on Hall Thruster Plume Properties