Experimental performance of a low-thrust, divergent-flow, contact-ionization electrostatic thruster.
- 1 May 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (5) , 610-615
- https://doi.org/10.2514/3.28917
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Ion propulsion system for stationary-satellite controlJournal of Spacecraft and Rockets, 1964
- Charge Transfer between Positive Cesium Ions and Cesium AtomsPhysical Review B, 1962
- Currents Limited by Space Charge between Coaxial CylindersPhysical Review B, 1923