Electric Thruster for Spacecraft with Mass up to 3000 kg
High specific impulse Hall thruster (72 mN, 1.65 kW, Isp 2680 s, 6 kg) for 3000 kg spacecraft; flight set delivered.
Technical specifications
- Purpose
- Propulsion system of spacecraft with mass up to 3000 kg
- Year of release
- 2011
- Guaranteed service life (GEO)
- 15 years
- Estimated production/delivery time
- 12 months
- Flight qualification
- Flight set delivered to customer
- Customization
- Can be adapted to customer requirements
- Thruster type
- Hall-effect
- Thrust
- 72 mN
- Power
- 1.65 kW
- Specific impulse
- 2680 s
- Cathode emitter
- W-Ba
- Mass
- 6 kg
- Designed service life
- More than 4000 hours
- TRL
- 8
About
This Hall-effect electric thruster is designed for the propulsion system of spacecraft with mass up to 3000 kg, offering high specific impulse of 2680 s at 72 mN thrust and 1.65 kW power. It features cathodes based on W-Ba emitters and was released in 2011. A flight set has been delivered to a customer (pre-qualification stage). Mass is 6 kg, designed service life more than 4000 hours. Adaptable to customer requirements.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
