System Tradeoffs for Pulsed MPD Thruster in Space Mission Application
- 1 December 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (12) , 858-862
- https://doi.org/10.2514/3.61812
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Performance of Quasi-Steady MPD Thrusters at High PowersAIAA Journal, 1972
- Large Impulses of Self-Magnetic OriginJournal of Applied Physics, 1971
- System requirements for application of a pulsed MPD to electrical propulsionJournal of Spacecraft and Rockets, 1969
- Quasi-steady plasma accelerationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Investigations on plasma thrusters with thermal and self-magnetic acceleration.AIAA Journal, 1967