SPS-40 Propulsion System
The SPS-40 Propulsion System is designed for a power consumption of 300-500 W and can provide a total impulse of up to 350 kN∙s. SPS-40 consists of ST-40 Hall-effect Thruster(s), Xenon storage and feed system, Power Processing Unit (PPU). With the help of its characteristics, SPS-40 is able to adjust the orbit parameters, ensure the maneuverability and deorbiting of a wide range of satellites in space.
Specifications
Input power, W
300-500
Thrust, mN
15–29
Dry Mass (without tank), kg
9,2
Total impulse, kN∙s (one thruster configuration)
350
SPS-40
Propulsion System
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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.
