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An experimental investigation of the internal magnetic field topography of an operating Hall thruster

dc.contributor.authorPeterson, Peter Y.en_US
dc.contributor.authorGallimore, Alec D.en_US
dc.contributor.authorHaas, James M.en_US
dc.date.accessioned2010-05-06T21:51:57Z
dc.date.available2010-05-06T21:51:57Z
dc.date.issued2002-10en_US
dc.identifier.citationPeterson, Peter Y.; Gallimore, Alec D.; Haas, James M. (2002). "An experimental investigation of the internal magnetic field topography of an operating Hall thruster." Physics of Plasmas 9(10): 4354-4362. <http://hdl.handle.net/2027.42/70249>en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/70249
dc.description.abstractMagnetic field measurements were made in the discharge channel of the 5 kW-class P5 laboratory-model Hall thruster to investigate what effect the Hall current has on the static, applied magnetic field topography. The P5 was operated at 1.6 and 3.0 kW with a discharge voltage of 300 V. A miniature inductive loop probe (B-Dot probe) was employed to measure the radial magnetic field profile inside the discharge channel of the P5 with and without the plasma discharge. These measurements are accomplished with minimal disturbance to thruster operation with the High-speed Axial Reciprocating Probe system. The results of the B-Dot probe measurements indicate a change in the magnetic field topography from that of the vacuum field measurements. The measured magnetic field profiles are then examined to determine the possible nature and source of the difference between the vacuum and plasma magnetic field profiles. © 2002 American Institute of Physics.en_US
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dc.publisherThe American Institute of Physicsen_US
dc.rights© The American Institute of Physicsen_US
dc.titleAn experimental investigation of the internal magnetic field topography of an operating Hall thrusteren_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelPhysicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumPlasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, College of Engineering, Ann Arbor, Michigan 48109en_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/70249/2/PHPAEN-9-10-4354-1.pdf
dc.identifier.doi10.1063/1.1507771en_US
dc.identifier.sourcePhysics of Plasmasen_US
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