TY - GEN
T1 - Segmented electrodes in annual and cylindrical hall thrusters
AU - Raitses, Y.
AU - Smirnov, A.
AU - Staack, D.
AU - Fisch, N. J.
PY - 2006
Y1 - 2006
N2 - In recent experiments, a 2 kW Hall thruster with segmented electrodes, which were made of an exceptionally low sputtering and low secondary electron emission carbon fiber velvet material, was operated in the discharge voltage range of 200 - 700 V. The comparison of the voltage-versus-current characteristics and plasma parameters of the Hall thruster with and without segmented electrodes indicates that the magnetic insulation of the segmented thruster improves with the discharge voltage at fixed magnetic field. The observations reported here also extend the regimes wherein the segmented Hall thruster can have a narrower plume than that of the conventional non-segmented thruster. The use of segmented electrodes is also studied for a miniaturized 100 W cylindrical Hall thruster. For an optimized variant of this thruster, we achieved performance improvements, including a 30-40% plume narrowing, reliable discharge initiation, and stable operation in the discharge voltage range of 50-600 V.
AB - In recent experiments, a 2 kW Hall thruster with segmented electrodes, which were made of an exceptionally low sputtering and low secondary electron emission carbon fiber velvet material, was operated in the discharge voltage range of 200 - 700 V. The comparison of the voltage-versus-current characteristics and plasma parameters of the Hall thruster with and without segmented electrodes indicates that the magnetic insulation of the segmented thruster improves with the discharge voltage at fixed magnetic field. The observations reported here also extend the regimes wherein the segmented Hall thruster can have a narrower plume than that of the conventional non-segmented thruster. The use of segmented electrodes is also studied for a miniaturized 100 W cylindrical Hall thruster. For an optimized variant of this thruster, we achieved performance improvements, including a 30-40% plume narrowing, reliable discharge initiation, and stable operation in the discharge voltage range of 50-600 V.
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M3 - Conference contribution
AN - SCOPUS:34249308145
SN - 1563478188
SN - 9781563478185
T3 - Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
SP - 1586
EP - 1592
BT - Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
Y2 - 9 July 2006 through 12 July 2006
ER -