SPS-25 Propulsion System
The SPS-25 Propulsion System is designed for small satellites up to 500 kg, enabling orbit adjustments and deorbiting maneuvers. It offers low mass and fast production capabilities.
Typed specifications18 values
Discloses 8 of 11 fields engineers filter by in this category (category median 3).
- Propulsion family
- electric datasheet p.2
- Mass
- 5 kg max · Dry mass (without tank) · datasheet p.2
- Thrust
- 14 mN max · datasheet p.2
- Specific impulse
- 1 500 s max · datasheet p.2
- Total impulse
- 75 000 N·s max · one thruster configuration · datasheet p.2
- Propellant
- Xenon datasheet p.2 Krypton
- Power consumption
- 120–275 W product page
- TRL
- 9 datasheet p.1
- Thruster technology
- Hall effect Hall-effect thruster ST-25 · datasheet p.1
- Power at thrust
- 275 W max · datasheet p.2 120 W min | 120 W min | 275 W max | 120–275 W total power consumption
- Flight heritage
- Flown on EOS SAT-1 satellite product page
- Satellite class
- smallsat 100-500 kg up to 500 kg · datasheet p.1
- Dry mass
- 5 kg max · without tank · datasheet p.1
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier8 lines, in the manufacturer's own wording
- Total power consumption
- 120-275 W
- Thrust
- Up to 14 mN (0.014 N)
- Dry mass (without tank)
- Up to 5 kg
- Total impulse
- Up to 75 kN*s (one thruster configuration)
- Flight heritage
- Flown on EOS SAT-1 satellite
- Propellant
- Xenon, Krypton
- Specific impulse
- Up to 1500 s
- TRL Level
- 9
About
The SPS-25 Propulsion System is engineered for small satellites with a mass of up to 500 kg. Its primary functions include adjusting the satellite’s position in orbit and facilitating deorbiting at the end of its operational lifespan. Key advantages of this propulsion system are its low mass, which is crucial for small satellite missions, and its fast production capabilities, allowing for quicker deployment and scalability. The system is a complete propulsion solution, not just a thruster, and is intended for integration into satellite platforms requiring precise orbital control and end-of-life disposal.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.