A study on simultaneous design of a Hall Effect Thruster and its low-thrust trajectory

Author:

Kwon Kybeom,Lantoine Gregory,Russell Ryan P.,Mavris Dimitri N.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. C.W. Clauss, D.L. Tilley, D.A. Barnhart, Benefits of low-power stationary plasma thruster propulsion for small satellites, In: Proceedings of the 9th AIAA/USC Conference on Small Satellites, 1995.

2. D. Milligan, D. Gestal, O. Camino, D. Estublier, C. Koppel, SMART-1 electric propulsion operations, In: Proceedings of the 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA-2004-3436, Fort Lauderdale, Florida, 11–14 July 2004.

3. J. Fisher, A. Wilson, D. King, S. Meyer, C. EngelBrecht, K. de Grys, L. Werthman, The development and qualification of a 4.5kW Hall thruster propulsion system for GEO satellite applications, In: Proceedings of the 27th International Electric Propulsion Conference, IEPC-01-010, Pasadena, California, 15–19 October 2001.

4. Examination of the Structure and Evolution of Ion Energy Properties of a 5kW Class Laboratory Hall Effect Thruster at Various Operational Conditions (Ph.D. dissertation);Gulczinski,1999

5. L. Biagioni, M. Saverdi, M. Andrenucci, Scaling and performance prediction of Hall effect thrusters, In: Proceedings of the 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2003-4727, Huntsville, Alabama, 20–23 July 2003.

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