lon-Thruster Propellant Utilization
- 1 July 1972
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (7) , 511-517
- https://doi.org/10.2514/3.61732
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- Some performance characteristics of divergent- field bombardment thrustersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Study and optimization of 15-cm Kaufman thruster dischargesJournal of Spacecraft and Rockets, 1970
- SERT II - Thruster system ground testingJournal of Spacecraft and Rockets, 1970
- SERT II - Mission and experimentsJournal of Spacecraft and Rockets, 1970
- Nonuniformity and grid erosion in an electron bombardment ion engineAIAA Journal, 1965
- Static Theory of Density and Potential Distribution in a Beam-Generated PlasmaJournal of Applied Physics, 1964
- PROBE MEASUREMENTS OF THE DISCHARGE IN AN OPERATING ELECTRON BOMBARDMENT ENGINEAIAA Journal, 1963