Research Article
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 |
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