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
Input power, W 250–600
Specific Impulse
Specific Impulse, s 1850
Thrust
Thrust, mN 14-28
Efficiency
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.

The ST-25 Hall Thruster is a modification of a Thruster with an Anode Layer.

PPU

The Power Processing Unit is one of the components of the SPS-40 and SPS-25 propulsion systems.

XFS

SETS is developing a modular Xenon Feed System (XFS) with significant reductions in mass and cost while increasing system reliability.