Abstract
Abstract
Accelerator grid hole shift is a critical reason for erosion failure of optic systems in ion thrusters, which may also cause an unexpected roll torque about the ion beam axis. A three-dimensional (3D) model of ion optics is developed based on a particle-in-cell Monte Carlo collision method to investigate the plasma dynamics and performance of radio frequency (RF) grid systems with misalignments of apertures, which are compared with those in the direct current (DC) grid system. For the benchmark case, the 3D model gives a better agreement with the experiments in the ion energy distribution function (IEDF) compared with the two-dimensional model from a previous publication, with 36.4% and 47.9% relative error reduction of the peak position and full width at half maximum (FWHM), respectively, indicating the effectiveness of the developed 3D model. Simulations show that in the RF grid system the ion beamlet is deflected in the direction opposite to the shift of the accelerator grid hole, while electrons move first in the hole shift direction, and then deflect in the opposite direction. The average ion beamlet deflection angle calculated is consistent with the predictions from linear optical theory in both the RF and DC grid system. The amplitude of beamlet deflection angle fluctuation with time decreases with the increase of RF frequency. When the grid holes shift, the ion beamlet will deflect with the divergence angle almost unchanged in the DC grid system, while the beamlet divergence angle increases in the RF grid system. When RF frequency is low, the big vortex-like structure in the electron velocity phase diagram breaks into small vortices, showing a reduced oscillation intensity. The hole shift also causes high-frequency oscillation in the shift direction. In terms of performance, the RF grid system is more sensitive to grid hole shift than the DC grid system.
Funder
Asia Pacific Space Cooperation Organization
Beihang University
National Natural Science Foundation of China
Defense Industrial Technology Development Program
Reference49 articles.
1. In-orbit demonstration of an iodine electric propulsion system;Rafalskyi;Nature,2021
2. QinetiQ’s T6 and T5 ion thruster electric propulsion system architectures and performances;Hutchins,2015
3. Twin engine tests of the T6 ion engine for ESA’s bepicolombo mercury mission;Rudwan,2011
4. Qualification of the T6 ion thruster for the BepiColombo mission to the planet mercury,2011
5. Initial flight test results of the LIPS-200 electric propulsion system on SJ-9A satellite,2013
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