Effects of an Internally-Mounted Cathode on Hall Thruster Plume Properties

Author:

Hofer Richard,Johnson Lee,Goebel Dan,Fitzgerald Dennis

Publisher

American Institute of Aeronautics and Astronautics

Reference33 articles.

1. Szabo, J., Azziz, Y. "Characterization of a High Specific Impulse Xenon Hall Effect Thruster," IEPC2005-324, 29th International Electric Propulsion Conference, Princeton University, 31 Oct - 4Nov 2005.

2. Pidgeon, D. J., Corey, R. L., Sauer, B., and Day, M. L. "Two Years On-Orbit Performance of SPT-100 Electric Propulsion," Proceedings of the 24th AIAA International Communications Satellite Systems Conference, AIAA Paper 2006-5353, San Diego, CA, June11-14,2006.

3. Yee, T. "Roadrunner, a high-performance responsive space mission," SSC04-I-5, 18thAnnual AIAA/USU Conference on Small Satellites, Utah State University, Logan, UT, Aug. 2004.

4. Bromaghim, D. R., Singleton, J. T., Gorecki, R., Dong Tan, F., Choy, H. et al. "200 W Hall Thruster Propulsion Subsystem Development for Microsatellite Missions," Proceedings of the 53rd JANNAF Propulsion Meeting, Monterey, CA, Dec.5-8,2005.

5. Welander, B., Carpenter, C., de Grys, K. H., Hofer, R. R., Randolph, T. M. et al. "Life and Operating Range Extension of the BPT-4000 Qualification Model Hall Thruster," Proceedings of the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2006-5263, Sacramento, CA, July9-12,2006.

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