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Use of Conjugate Gradient Methods for the Great-Circle Reduction
Development Toward a Spaceflight Capable VASIMR® Engine and SEP Applications (AIAA 2014-4173)
Using VASIMR® for the Proposed Europa Mission (AIAA 2014-4344)
SIMULATION OF ICRF PLASMA HEATING IN THE VASIMR EXPERIMENT
Performance Measurements and Technology Demonstration of the VASIMR® VX-200
Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
VX-200 Magnetoplasma Thruster Performance Results Exceeding Fifty-Percent Thruster Efficiency