Numerical Simulation of Interaction between Hall Thruster CEX Ions and SMART-1 Spacecraft

Table 1

Operating parameters of PPS-1350 Hall thruster.

Parameter	Value
Thrust	70 mN
Voltage	350 V
Ion current	3.8 A
Mass flow rate	4.2 mg/s
Specific impulse	164 s
Total efficiency	51%
Outer insulator diameter	100 mm
Inner insulator diameter	56 mm
Neutral temperature	750 K
Electron temperature	2 eV