Variable Specific Impulse Interplanetary Trajectory Design and Optimization (AAS 01-438)
Transport vehicle for manned Mars missions powered by inertial confinement fusion
EXHAUST PLUME SPATIAL STRUCTURE OF THE VASIMR® VX-200
The VASIMR(TM) VX-100 Engine: Next Step to High Power Electric Propulsion
High Power Ion Cyclotron Heating in the VASIMR Engine AIAA Paper
VASIMR(TM): A Private Enterprise Solution to Space Transportation Beyond LEO AIAA Paper
VASIMR VX-200: High Power Electric Propulsion for Space Transportation Beyond LEO
Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
VX-200 Magnetoplasma Thruster Performance Results Exceeding Fifty-Percent Thruster Efficiency