2006 48th Annual Meeting of the Division of Plasma Physics
Monday–Friday, October 30–November 3 2006;
Philadelphia, Pennsylvania
Session CI2: Plasma Technology: Plasma Thrusters, Plasma Discharges
2:00 PM–5:00 PM,
Monday, October 30, 2006
Philadelphia Marriott Downtown
Room: Grand Salon CDE
Chair: Valery Godyak, Sylvania
Abstract ID: BAPS.2006.DPP.CI2.1
Abstract: CI2.00001 : Experimental and theoretical studies of cylindrical Hall thrusters*
2:00 PM–2:30 PM
Preview Abstract
Abstract
Author:
Artem Smirnov
(Princeton Plasma Physics Laboratory)
The Hall thruster is a mature electric propulsion device that holds
considerable promise in terms of the propellant saving potential. The
annular design of the conventional Hall thruster, however, does not
naturally scale to low power. The efficiency tends to be lower, and the
lifetime issues are more aggravated. Cylindrical geometry Hall thrusters
have lower surface-to-volume ratio than conventional thrusters and, thus,
seem to be more promising for scaling down [Y. Raitses and N.J. Fisch,
\textit{Phys. Plasmas} \textbf{8}, 2579 (2001)]. The cylindrical Hall thruster (CHT) is
fundamentally different from the conventional design in the way the
electrons are confined and the ion space charge is neutralized. Both the
large (9 cm channel diam., 600 -- 1000 W) and miniaturized (2.6 cm channel
diam., 50 -- 300 W) CHTs exhibit performances comparable with those of the
state-of-the-art conventional (annular) design Hall thrusters of similar
sizes [A. Smirnov \textit{et al}., \textit{J. Appl. Phys}.\textbf{ 92}, 5673 (2002)]. A comprehensive
experimental and theoretical study of the CHT physics has been conducted,
addressing the questions of electron cross-field transport, propellant
ionization, plasma-wall interaction, and formation of the electron
distribution function. Probe measurements in the harsh plasma environment of
the micro thruster were performed. Several interesting effects, such as the
unusually high ionization efficiency and enhanced electron transport, were
observed [A. Smirnov \textit{et al.}, \textit{IEEE Trans. on Plasm. Sci}. \textbf{34}, 132 (2006)]. Kinetic simulations
suggest the existence of the strong fluctuation-enhanced electron diffusion
and predict the non-Maxwellian shape of the electron distribution function
[A. Smirnov \textit{et al.}, \textit{Phys. Plasmas} \textbf{11}, 4922 (2004)]. Through the acquired understanding
of the new physics, ways for further optimization of this means for
low-power space propulsion are suggested. Substantial flexibility in the
magnetic field configuration of the CHT is the key tool in achieving the
high-efficiency operation.
*Collaborators: Yevgeny Raitses and Nathaniel J. Fisch. This work was supported by grants from AFOSR, DARPA, and USDOE contract AC02-76CH0-3073.
To cite this abstract, use the following reference: http://meetings.aps.org/link/BAPS.2006.DPP.CI2.1