Numerical Study of Hall Thruster Plume and Sputtering Erosion

Table 1

Exit parameters of plasma plume.

Species	Xe	Xe^+	Xe^2+
Velocity, m/s	325	15000	21000
Temperature, K	1000	35000	35000
Number density, 10^17 m^−3	12.40	2.72	0.30