Research Article

Attitude Motion of Cylindrical Space Debris during Its Removal by Ion Beam

Table 3

Parameters of existing thrusters [15].

ParameterSPT100T100

Thrust84.9 mN82.4 mN
Discharge voltage300 V300 V
Discharge current4.5 A4.5 A
Power1350 W1390 W
Anode flow rate4.99 mg/s4.93 mg/s
Cathode flow rate0.38 mg/s0.41 mg/s
Specific impulse1610 s1570 s
Thrust efficiency49.7%47.1%