Preliminary Numerical Modelling of the Ionization Region to Model Ionic Propulsion

Ionic propulsion, where charged particles, ions, are produced between electrodes and
accelerate towards the negative electrode, has practical applications as a propulsion system
in the space industry; however, its adoption to in-atmosphere ionic propulsion is relatively
new and faces different challenges. A high potential difference is required to achieve a
corona discharge between a positive and negative electrode. In this work, we will explore
the feasibility of ionic propulsion using CFD modelling to replicate the effect of the ions,
with a future aim of improving efficiency. The ionization region is modelled for a 15 kV
potential difference, which is replicated with a velocity inlet, based on experimental data.
The output velocity from the numerical simulation shows the same trend as theoretical predictions
but significantly underestimates the magnitude of the ionic wind when compared
with theoretical estimates. Further modelling is highlighted to improve predictions and
assess if the theoretical model overestimates the ionic wind.