Reduced power processor requirements for the 30-cm diameter HG ion thruster
- 17 August 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- SERT II 1979 extended flight thruster system performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- HG ion thruster component testingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Electrical Prototype Power Processor for the 30-cm Mercury electric propulsion enginePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A mechanical, thermal and electrical packaging design for a prototype power management and control system for the 30 cm mercury ion thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Studies of internal sputtering in a 30-cm ion thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The evolution of the SEP stage /SEPS/ conceptPublished 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
- Solar electric propulsion breadboard thrust subsystem test resultsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- A 30-cm diameter bombardment thruster with a variable magnetic bafflePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Review of SERT II power conditioningJournal of Spacecraft and Rockets, 1971