Thrust Characteristics of High-Density Helicon Plasma Using Argon and Xenon Gases
Optimum design of power-limited propulsion systems with application to fast Earth-to-Mars transfer
Neutral Gas Expansion in a Cylindrical Helicon Discharge Chamber
to Mars: A Combined Robotic/Piloted Mars Mission
Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
Feasibility Assessment of Rapid Earth–Mars Transfers Using High-Power Electric Propulsion
Direct Thrust Measurement of an Electron Cyclotron Resonance Plasma Thruster
Characterization of Helicon Plasma Thruster Performance Operated for Various Rare Gas Propellants