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Title: Compact toroid formation using an annular helicon preionization source
Author (s): Stubbers, Robert A.
Jurczyk, Brian E.
Rovey, Joshua L.
Alman, Darren A.
Coventry, Matthew D.
Walker, Mitchell L. R.
Department/Lab Affiliations: Mechanical & Aerospace Engineering
Space Systems Engineering
Keywords: Helicon
Toroid
thruster
Issue Date: 2007-07
Publisher: American Institute of Aeronautics and Astronautics
Citation: Stubber, Robert A., Jurczyk, Brian E., Rovey, Joshua L., Alman, Darren A., and Walker, Mitchell L. R. "Compact Toroid Formation Using an Annular Helicon Preionization Source." AIAA-2007-5307, 43rd Joint Propulsion Conference, 2007.
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.
Type: Article - Journal
text
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titleCompact toroid formation using an annular helicon preionization source
contributor.authorStubbers, Robert A.
contributor.authorJurczyk, Brian E.
contributor.authorRovey, Joshua L.
contributor.authorAlman, Darren A.
contributor.authorCoventry, Matthew D.
contributor.authorWalker, Mitchell L. R.
contributor.deptlabMechanical & Aerospace Engineering
contributor.deptlabSpace Systems Engineering
subjectHelicon
subjectToroid
subjectthruster
date.issued2007-07
publisherAmerican Institute of Aeronautics and Astronautics
identifier.citationStubber, Robert A., Jurczyk, Brian E., Rovey, Joshua L., Alman, Darren A., and Walker, Mitchell L. R. "Compact Toroid Formation Using an Annular Helicon Preionization Source." AIAA-2007-5307, 43rd Joint Propulsion Conference, 2007.
identifier.pub.URI
http://pdf.aiaa.org/preview/CDReadyMJPC07_1492/PV2007_5307.pdf
description.abstractFormation 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.
typeArticle - Journal
type.DCMITypetext
rightsThis material is presented to ensure timely dissemination of scholarly and technical work. Copyright and all rights therein are retained by authors or by other copyright holders. All persons copying this information are expected to adhere to the terms and constraints invoked by each author's copyright. In most cases, these works may not be reposted without the explicit permission of the copyright holder.
rights.URI
http://www.aiaa.org/pdf/home/authorkit.pdf
date.accessioned2008-05-20T14:50:42Z
date.available2008-05-30T18:35:13Z
identifier.persist.URI
http://scholarsmine.mst.edu/post_prints/CompactToroidFormationUsingAnAnnularHeliconPr_09007dcc805027c0.html