Research Article
Attitude Motion of Cylindrical Space Debris during Its Removal by Ion Beam
Table 3
Parameters of existing thrusters [
15].
| Parameter | SPT100 | T100 |
| Thrust | 84.9 mN | 82.4 mN | Discharge voltage | 300 V | 300 V | Discharge current | 4.5 A | 4.5 A | Power | 1350 W | 1390 W | Anode flow rate | 4.99 mg/s | 4.93 mg/s | Cathode flow rate | 0.38 mg/s | 0.41 mg/s | Specific impulse | 1610 s | 1570 s | Thrust efficiency | 49.7% | 47.1% |
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