Electron bombardment propulsion system characteristics for large space systems
- 14 November 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Evolution of the satellite solar power station /SSPS/ conceptJournal of Spacecraft and Rockets, 1976
- Modular thrust subsystem approaches to solar electric propulsion module designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- 30 cm Engineering Model thruster design and qualification testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The advantages of the high voltage solar array for electric propulsionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Design, fabrication, and operation of dished accelerator grids on a 30-cm ion thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- An Experimental Investigation of a High-Voltage Electron-Bombardment Ion ThrusterJournal of the Electrochemical Society, 1969