A Comparison of 2-D Hybrid Hall Thruster Model to Experimental Measurements-Reference-Cited by-同舟云学术

A Comparison of 2-D Hybrid Hall Thruster Model to Experimental Measurements

Published:2004-06-21 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Allis Michelle¹,Gascon Nicolas¹,Fernandez Eduardo²,Vialard-Goudou Caroline¹,Cappelli Mark¹

Affiliation:

1. Stanford University

2. Eckerd College

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3951

Reference10 articles.

1. 1Fernandez,E.,Cappelli,M.A.,Mahesh,K."2DSimulationsofHallThrusters,"CTRAnnualResearchBriefs,1998,pp.81.

2. 3Fife, J. M. "Nonlinear Hybrid-PIC Modeling and Electrostatic Probe Survey of Hall Thrusters," Ph.D. Dissertation, Aeronautics and Astronautics Dept.,MassachusettsInstituteofTechnology, Cambridge, MA,1998.

3. Plasma Physics via Computer Simulation

4. 6Bohm, D, Burhop, E.H.S. Massey, H.S.W, "The Use of Probes for Plasma Exploration in Strong Magnetic Fields", in "The Characteristics ofElectrical Discharges in MagneticFields,"GuthrieA., WakerlingR.K., ed.McGraw-Hill, 1949, pp.13-76.

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