High-powered Electric Thruster for Spacecraft with Mass up to 3000 kg
Multimode Hall thruster (200/380 mN, 3.5/6 kW, Isp 1700/2650 s, 8 kg) for 3000 kg spacecraft, qualification model.
Technical specifications
- Purpose
- Propulsion system of spacecraft with mass up to 3000 kg
- Year of release
- 2001
- Guaranteed service life (GEO)
- 15 years
- Estimated production/delivery time
- 12 months
- Flight qualification
- Qualification model stage
- Customization
- Can be adapted to customer requirements
- Thruster type
- Hall-effect, multimode
- Thrust (modes)
- 200 mN / 380 mN
- Power (modes)
- 3.5 kW / 6.0 kW
- Specific impulse (modes)
- 1700 s / 2650 s
- Cathode emitter
- W-Ba
- Mass
- 8 kg
- Designed service life
- More than 6000 hours
- TRL
- 7
About
The High-powered Electric Thruster for Spacecraft with Mass up to 3000 kg is a multimode Hall-effect thruster with W-Ba cathode emitters for the propulsion system of 3000 kg-class spacecraft. It can operate in two modes: 200 mN / 3.5 kW (Isp 1700 s) or 380 mN / 6.0 kW (Isp 2650 s). Mass is 8 kg with a designed service life of more than 6000 hours. Released in 2001, currently at qualification model stage. Adaptable to customer requirements.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
