- Energy Efficiency in Low Voltage Hall Thrusters Jerry L. Ross
- Technical Notes TECHNICAL NOTES are short manuscripts describing new developments or important results of a preliminary nature. These Notes should not exceed 2500
- AIAA-2005-4232 AIAA/ASME/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 10-13 July 2005, Tucson, Arizona
- AIAA 2006-1891 CHARGE DETERMINATION FOR
- AIAA-2004-3768 American Institute of Aeronautics and Astronautics
- Regenerable Field Emission Cathode for Spacecraft Neutralization
- Laser-cooled ion plasmas in Penning traps J J Bollinger , J M Kriesel+
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- International Electric Propulsion Conference, University of Michigan, USA September 20 24, 2009
- International Electric Propulsion Conference, University of Michigan, USA September 20 24, 2009
- AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2-5 August 2009, Denver, Colorado
- Hall-Effect Thruster Cathode Coupling Part I: Efficiency Improvements from an Extended Outer Pole
- Hall-Effect Thruster Cathode Coupling Part II: Ion Beam and Near-Field Plume
- American Institute of Aeronautics and Astronautics Characterization of the Plasma Plume from a LaB6
- American Institute of Aeronautics and Astronautics Operating Characteristics of a Re-generable Field Emission
- Effect of Cathode Position on Hall-Effect Thruster Performance and Cathode Coupling Voltage
- American Institute of Aeronautics and Astronautics Performance Characterization and Ion Energy Analysis of a 2-kW Hall
- Steered Spacecraft Deployment Using Interspacecraft Coulomb Forces Gordon G. Parker, Lyon B. King and Hanspeter Schaub
- International Electric Propulsion Conference, Princeton University, October 31 November 4, 2005
- International Electric Propulsion Conference, Princeton University, October 31 November 4, 2005
- Vertically Aligned Carbon Nanotubes as the Sputter Resist in Space Propulsive Yoke Khin Yap, 1,*
- Paper No. AIAA-2004-6119. AIAA Space 2004 Conference, San Deigo, CA, Sept. 28-30, 2004. American Institute of Aeronautics and Astronautics
- THE EFFECT OF SEGMENTED ANODES ON THE PERFORMANCE AND PLUME OF A HALL THRUSTER
- Emission Cross Sections for Neutral Xenon Impacted by Xe+
- CONTROLLED SPACECRAFT CHARGING FOR COULOMB FORCE CONTROL OF SPACECRAFT FORMATIONS
- 1 1. Introduction
- American Institute of Aeronautics and Astronautics Re-generable Field Emission Cathodes for Low-Power
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- International Electric Propulsion Conference, Princeton University, October 31 November 4, 2005
- American Institute of Aeronautics and Astronautics Preliminary Sputter-erosion Characterization of Multiwalled
- American Institute of Aeronautics and Astronautics Performance Characteristics of a LaB6
- COULOMB FORCE VIRTUAL SPACE G. G. Parker, H. Schaub, A. Natarajan and L. B. King
- Efficiency Analysis of a Low Discharge Voltage Hall Jerry L. Ross
- Testing Multiwall Carbon Nanotubes on Ion Erosion for Advanced Space Yoke Khin Yap 1,*
- American Institute of Aeronautics and Astronautics Characterization of Near Field Plasma Environment of a
- International Electric Propulsion Conference IEPC-2007-153
- American Institute of Aeronautics and Astronautics Mobility Studies of a Pure Electron Plasma
- The 31st International Electric Propulsion Conference, University of Michigan, USA September 20 24, 2009
- AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit AIAA-2005-4236 10-13 July 2005, Tucson, Arizona
- International Electric Propulsion Conference, Princeton University, October 31 November 4, 2005
- TRANSPORT-PROPERTY AND MASS SPECTRAL MEASUREMENTS IN THE PLASMA EXHAUST PLUME OF A
- Ionization Efficiency in Electric Propulsion Devices Jerry L. Ross
- Hall-Effect ThrusterCathode Coupling The Effect of Cathode Position and Magnetic Field Topology
- Re-generable Field Emission Cathodes Part II: Quenched Emitter Performance Analyses
- Gridded retarding pressure sensor for ion and neutral particle analysis in flowing plasmas
- Effect of Cathode Position on Hall-Effect Thruster Performance and Cathode Coupling Voltage
- American Institute of Aeronautics and Astronautics Design and Construction of an Electron Trap for Studying Cross-
- CHALLENGES AND PROSPECTS OF COULOMB SPACECRAFT FORMATIONS
- Numerical Optimization of an Annular Field Reversed Configuration Translation Experiment
- AIAA-2002-3671 American Institute of Aeronautics and Astronautics
- American Institute of Aeronautics and Astronautics An Optical Diagnostic for Xenon Hall Thrusters Including Metastable
- Re-generable Field Emission Cathodes Part I: Surface Morphology of Emitter Apex
- Development of a Direct Evaporation Bismuth Hall Thruster Dean Richard Massey
- American Institute of Aeronautics and Astronautics Energetics of Propellant Options for High-Power Hall Thrusters
- Effect of Cathode Position on Hall-Effect Thruster Performance and Near-Field Plume Properties
- American Institute of Aeronautics and Astronautics Effects of Neutral Density on Electron Temperature and
- 40th Joint Propulsion Conference, Fort Lauderdale, FL, July 11-14, 2004 Effect of Segmented Anodes On the Beam Profile of a
- Re-generable Field Emission Cathodes for Electric Propulsion
- Regenerable Field Emission Cathodes: Surface Morphology and Performance
- The 32nd International Electric Propulsion Conference, Wiesbaden, Germany September 11-15, 2011
- The 32nd International Electric Propulsion Conference, Wiesbaden, Germany September 11 15, 2011
- The 32nd International Electric Propulsion Conference, Wiesbaden, Germany September 11 15, 2011
- King, Feirstine, Hohnstadt 1 25th Annual AIAA/USU
- Probe Studies of a Hall Thruster at Low Voltages
