Electric propulsion devices of using xenon propellant are nowadays widely adopted
for the space missions. A collisional-radiative (CR) model of xenon needs to be
developed to understand the kinetic mechanisms of the excited and energetic
species in these devices and also to support their optical diagnostics.
Previously, due to limitations in the fundamental cross section data, Xe CR
models focused on the atomic species; the ionic species, which also play
important roles for the thrusters, were not studied in detail. In our previous
paper, a fully relativistic Dirac B-spline
R-matrix method was applied to calculate the relevant cross
sections for electron collisions with the Xe+ ion. Based on
these data, a comprehensive CR modelโwith the kinetics of metastable and
excited levels of both Xe and Xe+ includedโcould be built.
The calculated density distributions of atomic and ionic levels are examined by
optical measurements in Hall thrusters in all of the four typical regions
(near-anode-, ionization-, acceleration-, and plume-region). The special kinetic
behaviors of the excited species are analyzed, and a set of rate coefficient
data used for the Xe CR model is also provided.