Formation and neutralization of electric charge and current of an ion thruster plume

J Perales-Díaz, F Cichocki, M Merino… - … Sources Science and …, 2021 - iopscience.iop.org
A 3D hybrid model is introduced and applied to the simulation of the xenon plasma plume
extraction, formation, and neutralization in a gridded ion thruster. The acceleration voltage is …

Design of the Retarding Potential Analyzer to be used with BURFIT-80 Ion Thruster and Validation using PIC-DSMC Code

M Satir, F Sik, E Turkoz, M Celik - 2015 7th international …, 2015 - ieeexplore.ieee.org
For better integration of plasma thrusters into spacecraft and satellites, potential damaging
effects of impinging high energy ions on the spacecraft surfaces should be taken into …

Evaluation of ion beam behavior in 50 W class RF ion thruster

HTT Nguyen, HD Vu, J Shin - International Journal of …, 2021 - Wiley Online Library
Phenomenological behavior of ion beam acceleration through the grid system in 50 W class
RF ion thruster has been investigated using PIC simulation and evaluated by experimental …

[PDF][PDF] Development and application of PICLas for combined optic-/plume-simulation of ion-propulsion systems

T Binder - 2019 - elib.uni-stuttgart.de
Electric propulsion systems are an efficient option for altitude/attitude control and orbit
transfers of spacecraft. One example is the gridded ion thruster which ionizes the propellant …

[PDF][PDF] ION OPTICS SYSTEM ANALYSIS OF THE RF-ICP ION THRUSTER

E Bozkurt, ÜE Güngör, N Alemdaroğlu - researchgate.net
This work presents the theoretical analysis of ion optics system (IOS) of the two-gridded
RFICP ion thruster. The simulations of this system are done by using the COMSOL …