ST-25 Hall Thruster

The ST-25 Hall Thruster is the most compact and based on the permanent magnet in the central core. It is designed with the latest modern manufacturing principles that make ST-25 a perfect solution for satellite constellations. The high standards of manufacturing and technology allowed the ST-25 thruster to operate successfully on board the spacecraft and show excellent performance.

Specifications
Input power
Input power, W 100-250
Thrust
Thrust, mN 5-14
Specific Impulse
Specific Impulse, s 1000-1500
Efficiency
Efficiency, % 38
ST-25 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-100 Hall Thruster with an anode layer is designed for use as part of the propulsion system for satellites mass up to 1 T.

The ST-40 Hall Thruster with an anode layer is designed for use as part of the propulsion system for satellites mass up to 1 T.

PPU

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

The Power Processing Unit (PPU) is designed as a part of the Electric Propulsion System (EPS) SPS-25, which consists of ST-25 Hall Thruster and Xenon Feed System (XFS).

XFS

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