SPS-40 Propulsion System
The SPS-40 Propulsion System leverages the leading-edge Hall thrusters and is optimized for small mass class satellites. The main objectives are to adjust the positions of satellites and deorbit after the finish of their operational lifespan. Designed with state-of-the-art Hall thruster technology based on permanent magnets delivering superior performance, and is a significant step forward to miniaturize thrusters without reliability compromise.
Specifications
Input power, W
300-600
Thrust, mN
15–28
Weight, kg
13,8
Total impulse, kN (one thruster configuration)
350
SPS-40
Propulsion System
/
Other systems
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 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).
SETS is developing a modular Xenon Feed System (XFS) with significant reductions in mass and cost while increasing system reliability.
