Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
VX-200 Magnetoplasma Thruster Performance Results Exceeding Fifty-Percent Thruster Efficiency
Helicon Mode and Xenon Operation with the Nonambipolar Electron Source AIAA Paper
VASIMR®: Deep Space Transportation for the 21st Century
EXHAUST PLUME SPATIAL STRUCTURE OF THE VASIMR® VX-200
VASIMR Vx-100: High Power Electric Propulsion for Space Transportation Beyond LEO
Hall Thruster and VASIMR VX-100 Force Measurements using a Plasma Momentum Flux Sensor
High Power Electric Propulsion Using VASIMR™: Results from Flight Prototypes
The VASIMR(TM) VX-100 Engine: Next Step to High Power Electric Propulsion
ISS Space Plasma Laboratory: An Orbital Solar and Heliospheric Physics Simulation Facility
Performance Measurements and Technology Demonstration of the VASIMR® VX-200
VASIMR VX-200: High Power Electric Propulsion for Space Transportation Beyond LEO