Propellant Utilization in Hall Thrusters
- 1 March 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 14 (2), 247-253
- https://doi.org/10.2514/2.5274
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Discharge characteristics of Hall current acceleratorsPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- End-of-life Stationary Plasma Thruster far-field plume characterizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Earth-to-moon transfer with a limited power engineJournal of Guidance, Control, and Dynamics, 1995
- Investigations of a laboratory model Hall thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995