A 30-cm diameter argon ion source
- 16 August 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Electron bombardment propulsion system characteristics for large space systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Nonpropulsive applications of ion beamsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Optimization of an electron-bombardment ion source for ion machining applicationsJournal of Vacuum Science and Technology, 1975
- 30 cm Engineering Model thruster design and qualification testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Measurement of beam divergence of 30-centimeter dished gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Performance of 30-cm ion thrusters with dished accelerator gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- High voltage pulse ignition of mercury discharge hollow cathodesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Studies of dished accelerator grids for 30-cm ion thrustersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Ion-Beam Techniques for Device FabricationJournal of Vacuum Science and Technology, 1971
- Performance and control of a 30-cm-diam, low-impulse, Kaufman thrusterJournal of Spacecraft and Rockets, 1970