Contour algorithms for a Hall Thruster Hybrid Code-Reference-Cited by-同舟云学术

Contour algorithms for a Hall Thruster Hybrid Code

Published:2006-07-09 Issue: Volume: Page:
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Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Anton Alfredo,Ahedo Eduardo

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. 3D. Escobar and E. Ahedo. Improved electron formulation for a Hall thruster hybrid code. In42th Joint Propulsion Conference, Sacramento, CA, AIAA-2006-4326. American Institute of Aeronautics and Astronautics,Washington, DC, 2006.

2. 4F.ParraamdE.Ahedo. ImprovingparticleaccuracyinaHallthrusterhybridcode, In42th Joint Propulsion Conference, Sacramento, CA, AIAA-2006-4830. American Institute of Aeronautics and Astronautics,Washington, DC, 2006.

3. 5D. Escobar, E. Ahedo, and F. I. Parra. On conditions at the sheath boundaries of a quasineutral code for Hall thrusters. InProc. 29th International Electric Propulsion Conference, Princeton, USA, IEPC-2005-041. Electric Rocket Propulsion Society, Fairview Park, OH, 2005.

4. 6I. Maqueda, A. Antón, E. Ahedo, Y. Raitses, and N. Fisch. Numerical simulations of a 2kW Hall thruster. In42th Joint Propulsion Conference, Sacramento, CA, AIAA-2006-4655. American Institute of Aeronautics and Astronautics,Washington, DC, 2006.

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4. Improvements On Particle Accuracy In A Hall thruster Hybrid Code;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

5. Numerical Simulations of a 2kW Hall Thruster;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09