Show simple item record

On the potential distribution in Hall thrusters

dc.contributor.authorKeidar, Michaelen_US
dc.contributor.authorGallimore, Alec D.en_US
dc.contributor.authorRaitses, Yevgenyen_US
dc.contributor.authorBoyd, Iain D.en_US
dc.date.accessioned2010-05-06T21:13:16Z
dc.date.available2010-05-06T21:13:16Z
dc.date.issued2004-09-27en_US
dc.identifier.citationKeidar, Michael; Gallimore, Alec D.; Raitses, Yevgeny; Boyd, Iain D. (2004). "On the potential distribution in Hall thrusters." Applied Physics Letters 85(13): 2481-2483. <http://hdl.handle.net/2027.42/69833>en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/69833
dc.description.abstractA model of the plasma flow in a Hall thruster channel is developed that takes into account the two-dimensional current conservation effect and relies on some experimental input parameters, such as magnetic field and electron temperature distribution. The model is an attempt to explain the experimentally found nonuniform potential distribution across the thruster channel. This effect is explained by the change of the electron mobility across a magnetic field due to the magnetic field gradient and due to the electron current along the magnetic field driven by the electron temperature gradient.en_US
dc.format.extent3102 bytes
dc.format.extent296174 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/octet-stream
dc.publisherThe American Institute of Physicsen_US
dc.rights© The American Institute of Physicsen_US
dc.titleOn the potential distribution in Hall thrustersen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelPhysicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109en_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109en_US
dc.contributor.affiliationotherPrinceton Plasma Physics Laboratory, Princeton, New Jersey 08543en_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/69833/2/APPLAB-85-13-2481-1.pdf
dc.identifier.doi10.1063/1.1797555en_US
dc.identifier.sourceApplied Physics Lettersen_US
dc.identifier.citedreferenceA. L. Morozov, Sov. Phys. Dokl. 10, 775 (1966).en_US
dc.identifier.citedreferenceA.I. Morozov and V.V. Savelyev, in Review of Plasma Physics, edited by B. B. Kadomtsev and V. D. Shafranov (Consultant Bureau, New York, 2000), Vol. 21, p. 203.en_US
dc.identifier.citedreferenceV. Kim, J. Propul. Power 14, 736 (1998).en_US
dc.identifier.citedreferenceV. V. Zhurin, H. R. Kaufman, and R. S. Robinson, Plasma Sources Sci. Technol. 8, 1 (1999).en_US
dc.identifier.citedreferenceM. Keidar, I. D. Boyd, and I. I. Beilis, Phys. Plasmas 9, 1675 (2001).en_US
dc.identifier.citedreferenceY. Raitses, M. Keidar, D. Staack, and N. J. Fisch, J. Appl. Phys. 92, 4906 (2002).en_US
dc.identifier.citedreferenceJ. M. Haas and A. D. Gallimore, IEEE Trans. Plasma Sci. 30, 687 (2002).en_US
dc.identifier.citedreferenceJ. M. Haas and A. D. Gallimore, Phys. Plasmas 8, 652 (2001).en_US
dc.identifier.citedreferenceT.B. Smith, D.A. Herman, A.D. Gallimore, and R.P. Drake, IEPC-01-019, 27th International Electric Propulsion Conference, Pasadena, CA, 15–19 October 2001.en_US
dc.identifier.citedreferenceM. Keidar, I. Beilis, R. L. Boxman, and S. Goldsmith, J. Phys. D 29, 1973 (1996).en_US
dc.identifier.citedreferenceL. Dorf, Y. Raitses, N. J. Fisch, and V. Semenov, Appl. Phys. Lett. 84, 1070 (2004).en_US
dc.owningcollnamePhysics, Department of


Files in this item

Show simple item record

Remediation of Harmful Language

The University of Michigan Library aims to describe library materials in a way that respects the people and communities who create, use, and are represented in our collections. Report harmful or offensive language in catalog records, finding aids, or elsewhere in our collections anonymously through our metadata feedback form. More information at Remediation of Harmful Language.

Accessibility

If you are unable to use this file in its current format, please select the Contact Us link and we can modify it to make it more accessible to you.