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Abstract
To suit a wide variety of space mission profiles, different designs of ion thrusters were developed, such as the HighâEfficiencyâMultistageâPlasma thrusters (HEMPâT). In the past, the optimization of ion thrusters was a difficult and timeâconsuming process and evolved experimentally. Because the construction of new designs is expensive, cheaper methods for optimization were soughtâafter. Computerâbased simulations are a cheap and useful method towards predictive modelling. The physics in HEMPâT requires a kinetic model. The ParticleâinâCell (PIC) method delivers selfâconsistent solutions for the plasmas of ion thrusters, but it is limited by the high amount of computing time required to study a specific system. Therefore, it is not suited to explore a wide operational and design space. An approach to decrease computing time is selfâsimilarity scaling schemes, which can be derived from the kinetic equations. One specific selfâsimilarity scheme is investigated quantitatively in this work for selected HEMPâTs, using PIC simulations. The possible application of the scaling is explained and the limits of this approach are derived.