Investigation of hollow cathode performance for 30-cm thrusters
- 16 August 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Component testing of a 30-centimeter diameter electron bombardment thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- A Mercury plasma-bridge neutralizer.Journal of Spacecraft and Rockets, 1968