Effects of propellant and electrode geometry on pulsed ablative plasma thruster performance
- 19 March 1975
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A flight qualified pulsed electric thruster for satellite controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Pulsed plasma microthruster propulsion system for synchronous orbit satelliteJournal of Spacecraft and Rockets, 1970