Design of a thrust stand for high power electric propulsion devices
- 12 July 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Performance of a 100 kW class applied field MPD thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Effect of background pressure on magnetoplasmadynamic thruster operationJournal of Spacecraft and Rockets, 1970