Further Development and Preliminary Results of the AQUILA Hall Thruster Plume Model-Reference-Cited by-同舟云学术

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Further Development and Preliminary Results of the AQUILA Hall Thruster Plume Model

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Santi Mark¹,Cheng Shannon¹,Celik Murat¹,Martinez-Sanchez Manuel¹,Peraire Jaime¹

Affiliation:

1. Massachusetts Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4873

Reference5 articles.

1. The characteristics of the EP exhaust plume in space

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1. 3D Detailed Far Field Plume Modeling of SPT-100;AIAA Propulsion and Energy 2019 Forum;2019-08-16

2. Collisionless electron cooling in unmagnetized plasma thruster plumes;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

3. SM/MURF: Current Capabilities and Verification as a Replacement of AFRL Plume Simulation Tool COLISEUM;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

4. Experimental and Numerical Examination of the BHT-200 Hall Thruster Plume;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

5. Comparison of Hall Thruster Plume Expansion Model with Experimental Data;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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