TY - GEN
T1 - Modeling and development of the rf-controlled hollow cathode concept
AU - Plasek, Matthew L.
AU - Wordingham, Christopher J.
AU - Choueiri, Edgar Y.
N1 - Publisher Copyright:
© 2013, American Institute of Aeronautics and Astronautics Inc. All rights reserved.
PY - 2013
Y1 - 2013
N2 - A promising new hollow cathode concept for high-power, long-lifetime electric thruster applications is explored using finite-element analysis to inform an experiment presently being constructed. This RF-Controlled Hollow Cathode concept adds radio-frequency power to a large-diameter cathode. To explore the concept’s feasibility and behavior, numerical simulations were performed with a simplified two-dimensional model which captures the plasma, the thermionic emission, and the added RF power. It was found that by increasing the RF power, the centerline plasma density profile increased and its peak shifted upstream, resulting in enhanced thermionic emission from a greater emitter area, and thus supporting the promise of the concept for high-power, long-lifetime applications. It was also observed that a pronounced “jump” occurs in the plasma density and other parameters at a critical RF power, and its occurrence is strongly dependent on gas pressure. This beneficial jump behavior was attributed to a cavity resonance effect caused by the RF waves constructively interfering to sharply increase the electric field amplitude at a critical RF electric field phase and RF-reflecting plasma density depth.
AB - A promising new hollow cathode concept for high-power, long-lifetime electric thruster applications is explored using finite-element analysis to inform an experiment presently being constructed. This RF-Controlled Hollow Cathode concept adds radio-frequency power to a large-diameter cathode. To explore the concept’s feasibility and behavior, numerical simulations were performed with a simplified two-dimensional model which captures the plasma, the thermionic emission, and the added RF power. It was found that by increasing the RF power, the centerline plasma density profile increased and its peak shifted upstream, resulting in enhanced thermionic emission from a greater emitter area, and thus supporting the promise of the concept for high-power, long-lifetime applications. It was also observed that a pronounced “jump” occurs in the plasma density and other parameters at a critical RF power, and its occurrence is strongly dependent on gas pressure. This beneficial jump behavior was attributed to a cavity resonance effect caused by the RF waves constructively interfering to sharply increase the electric field amplitude at a critical RF electric field phase and RF-reflecting plasma density depth.
UR - http://www.scopus.com/inward/record.url?scp=84913596655&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84913596655&partnerID=8YFLogxK
U2 - 10.2514/6.2013-4036
DO - 10.2514/6.2013-4036
M3 - Conference contribution
AN - SCOPUS:84913596655
SN - 9781624102226
T3 - 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
BT - 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013
Y2 - 14 July 2013 through 17 July 2013
ER -