Full Particle-In-Cell Simulation Methodology for Axisymmetric Hall Effect Thrusters-Reference-Cited by-同舟云学术

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Full Particle-In-Cell Simulation Methodology for Axisymmetric Hall Effect Thrusters

Published:2014-01 Issue:1 Volume:30 Page:197-208
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Szabo James¹,Warner Noah²,Martinez-Sanchez Manuel³,Batishchev Oleg⁴

Affiliation:

1. Busek Company, Inc., Natick, Massachusetts 01760

2. Surface Systems Engineering, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

3. Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

4. Physics Department/Center for Interdisciplinary Research on Complex Systems, Northeastern University, Boston, Massachusetts 02115

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34774

Reference64 articles.

1. The conceptual development of stationary plasma thrusters

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