Increased capabilities of the 30-cm diameter Hg ion thruster
- 8 May 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Ion beam divergence characteristics of three-grid accelerator systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Sensitivity of 30-cm mercury bombardment ion thruster characteristics to accelerator grid designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Effect of facility background gases on internal erosion of the 30-cmHg ion thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A 30-cm diameter argon ion sourcePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Measurement of beam divergence of 30-centimeter dished gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- The advantages of the high voltage solar array for electric propulsionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- 12 centimeter magneto-electrostatic containment mercury ion thrusterdevelopmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971