Compact Toroid Formation Using an Annular Helicon Preionization Source
Abstract
Formation and ejection of compact plasma toroids for high-thrust and high-specific impulse applications are modeled in conjunction with experimental efforts for concept development. in particular, use of field-reversed configuration plasma with an annular helicon pre-ionization source is being investigated. This type of thruster would have high thrust and no need for electrodes or grids that limit lifetime and reliability. Results from modeling the pulsed power system, the FRC formation process, and acceleration indicate that the annular helicon pre-ionization source is ideal for FRC processes to maximize coupling between the pulsed field and the plasma.
Recommended Citation
R. A. Stubbers et al., "Compact Toroid Formation Using an Annular Helicon Preionization Source," Proceedings of the 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Joint Propulsion Conferences (2007, Cincinnati, OH), American Institute of Aeronautics and Astronautics (AIAA), Jul 2007.
The definitive version is available at https://doi.org/10.2514/6.2007-5307
Meeting Name
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Joint Propulsion Conferences (2007: Jul. 8-11, Cincinnati, OH)
Department(s)
Mechanical and Aerospace Engineering
Keywords and Phrases
Helicon; Toroid; Thruster
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2007 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
01 Jul 2007
