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.
Key figurescomparable across the catalogue
- Mass
- 5 kg
- Payload capacity
- 500 kg
- Power
- 120 W
- Thrust
- 0.014 N
- Total impulse
- 75,000 N·s
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- 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.