DocumentCode :
1950785
Title :
Magnetic field topography of the anode layer thruster
Author :
Domonkos, Matthew T. ; Gallimore, A.C.
Author_Institution :
Michigan Univ., Ann Arbor, MI, USA
fYear :
1997
fDate :
19-22 May 1997
Firstpage :
330
Lastpage :
331
Abstract :
Summary form only given. The anode layer thruster (TAL) built by the Central Scientific Research Institute of Machine Buildings (TsNIMASH) of Kaliningrad, Russia is currently being investigated in the US for both primary and auxiliary spacecraft propulsion. The TAC is a Hall accelerator which consists of an inner electromagnet, three outer electromagnets, an annular anode through which xenon propellant is supplied, and a hollow cathode neutralizer. The radial magnetic field created by the electromagnets crosses with the axial magnetic field to produce an azimuthal drift of electrons. The magnetic field has been mapped using water-cooled Hall probes both while the thruster was operating and with only the vacuum field generated by the electromagnets. The measured radial magnetic field strength decreased by approximately two-thirds during operation of the thruster. Preliminary estimates to determine the role of the azimuthal electron current indicated that nearly 800 A were required to effect this change. Additional experiments were conducted to examine the error in the Hall probe measurements and to investigate the nature of the decrease in magnetic field strength.
Keywords :
aerospace instrumentation; aerospace propulsion; anodes; electromagnetic launchers; magnetic field measurement; probes; space vehicles; 800 A; Central Scientific Research Institute of Machine Buildings; Hall accelerator; Hall probe measurements; Kaliningrad; Xe; Xe propellant; annular anode; anode layer thruster; axial magnetic field; azimuthal electron current; azimuthal electron drift; electromagnets; hollow cathode neutralizer; inner electromagnet; magnetic field strength; magnetic field topography; outer electromagnets; radial magnetic field; radial magnetic field strength; spacecraft propulsion; vacuum field; Anodes; Electromagnetic measurements; Electromagnets; Electrons; Hall effect devices; Magnetic field measurement; Magnetic fields; Propulsion; Space vehicles; Surfaces;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Plasma Science, 1997. IEEE Conference Record - Abstracts., 1997 IEEE International Conference on
Conference_Location :
San Diego, CA, USA
ISSN :
0730-9244
Print_ISBN :
0-7803-3990-8
Type :
conf
DOI :
10.1109/PLASMA.1997.605239
Filename :
605239
Link To Document :
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