ST-40 hall-effect thruster
The ST-40 Hall-Effect Thruster with an anode layer is designed for use as part of the propulsion system for satellites mass up to 1 T. It is used to orient and stabilize of the spacecraft in various orbits. The propulsion system provides a thrust of up to 28 mN at a maximum electric power consumption of 600 W. The propulsion system that contains ST-40 can be used on satellites for various purposes.
Input power, W
250–600
Specific Impulse, s
1850
Thrust, mN
14-28
Efficiency, %
40
ST-40
hall thruster
/
Other systems
The SPS-40 Propulsion System was designed for medium and large satellites and able to adjust the orbit parameters and insure the maneuverability of satellites in space.
The SPS-25 Propulsion System was designed for mini satellites mass up to 500 kg.
SETS is developing a modular Xenon Feed System (XFS) with significant reductions in mass and cost while increasing system reliability.
