SPS-100 Propulsion System

The SPS-100 Propulsion System is designed for medium and large satellites that can provide power to the propulsion system from 1000 W to 1600 W. The SPS-100 is a perfect solution for a wide range of spacecraft and can be used for orbit maintenance, performing orbital maneuvers and deep space missions. SPS-100 consists of ST-100 Hall-effect Thruster(s), Xenon storage and feed system, Power processing unit.

Specifications
Input power
Input power, W Up to 1600
Thrust
Thrust, mN Up to 90
Mass
Dry Mass (without tank), kg Up to 20
Total impulse
Total impulse, MN∙s (one thruster configuration) Up to 3
SPS-100 Propulsion System

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.

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.

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.