The IPG6-B as a research facility to support future development of electric propulsion
Fully kinetic study of facility pressure effects on RF-source magnetic nozzles
The performance of a magnetic nozzle enhanced magnetoplasmadynamic thruster
Los Alamos Research in Nozzle Based Coaxial Plasma Thrusters
Open-Front Approach of a Microwave Rocket Sustained by a Resonant Magnetic Field
Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
A novel fusion approach to space power and propulsion