Electric Thruster for Spacecraft with Mass up to 2500-3000 kg
Hall-effect electric thruster (95 mN, <2.4 kW, Isp 2680 s, 5.25 kg) for 2500–3000 kg spacecraft, record specific impulse.
Technical specifications
- Purpose
- Propulsion system of spacecraft with mass up to 2500-3000 kg
- Year of release
- 2018
- Guaranteed service life (GEO)
- 15 years
- Estimated production/delivery time
- 12 months
- Flight qualification
- Qualification model stage (not yet flight-qualified)
- Customization
- Can be adapted to customer requirements
- Thruster type
- Hall-effect
- Thrust
- 95 mN
- Power
- Less than 2.4 kW
- Specific impulse
- 2680 s
- Mass
- 5.25 kg
- Designed service life
- More than 6000 hours
- TRL
- 7
About
This Hall-effect electric thruster is designed for the propulsion system of spacecraft with mass up to 2500–3000 kg. It delivers 95 mN thrust at less than 2.4 kW power consumption with a specific impulse of 2680 s — described as a record specific impulse for Hall-effect thrusters — and is designed for more than 6000 hours of operation. Mass is 5.25 kg. Released in 2018; currently at qualification model stage, not yet flight-qualified. Adaptable to customer requirements.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
