High-Fidelity Particle-In-Cell Simulations of Ion Thruster Optics IEPC-2017-451
High-Fidelity Particle-In-Cell Simulations of Ion Thruster Optics IEPC-2017-451
复制标题
离子推进器光学器件的高保真粒子内模拟 IEPC-2017-451
DOI:
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发表时间:
2017
期刊:
影响因子:
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通讯作者:
S. Fasoulas
中科院分区:
文献类型:
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作者:
T. Binder;M. Pfeiffer;S. Fasoulas
The numerical simulation of ion thruster optics is one of the most common applications of particle-based methods in the field of electric propulsion. Over the years, powerful tools for simulation of ion trajectories and charge exchange erosion have been developed and validated. The validity of prediction results is high as long as the ion optics system is operated far from the electron back-streaming (EBS) limit. Operating gridded ion thrusters with EBS is one of the most dangerous failure modes, a fully kinetic numerical modeling is therefore highly desirable. For this, a more sophisticated approach based on high fidelity Particle-In-Cell (PIC) methods is expected to be necessary, capable to realistically handle the different scales of heavy ions and very low mass electrons. In this paper, electrostatic optics simulations of a RIT-μX thruster are conducted. The results are compared with simulations assuming the common Boltzmann relation. The spatial distributions of electric potential and number densities as well as the determined back-streaming currents match well. The velocity distribution functions of electrons correspond at most positions to thermal equilibrium. The comparison between simulations of the actual thruster and a corresponding infinite pattern of grid apertures show that the state at edge apertures differs only slightly. The experimentally determined EBS threshold, however, could not be reproduced, which is probably caused by various assumptions made for the simulation parameters.