Design model for the baffle aperture region of a hollow cathode thruster
- 21 April 1981
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Plasma processes in inert gas thrustersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Electron diffusion through the baffle aperture of a hollow cathode thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Plasma property and performance prediction for mercury ion thrustersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Plasma properties and performance of mercury ion thrustersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Anomalous Diffusion of a Plasma across a Magnetic FieldPhysics of Fluids, 1962
- Reliability of Probe Measurements in Hot Cathode Gas DiodesJournal of Applied Physics, 1952