Study and optimization of 15-cm Kaufman thruster discharges
- 1 January 1970
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 7 (1) , 26-30
- https://doi.org/10.2514/3.29858
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Radial field Kaufman thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Magneto-electrostatically contained plasma ion thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Performance of a 15-centimeter diameter, hollow-cathode Kaufman thrustorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- PROBE MEASUREMENTS OF THE DISCHARGE IN AN OPERATING ELECTRON BOMBARDMENT ENGINEAIAA Journal, 1963