SPS-25 Propulsion System
Compact electric propulsion system for small satellites up to 500 kg, flight-proven on EOS SAT-1.
Technical specifications
- 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
About
The SPS-25 is designed for small satellites up to 500 kg, used to adjust satellite positions and deorbit them at end of operational life. Its advantages include low mass and fast production capability. The system has flight heritage, having flown on the EOS SAT-1 satellite.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.