Electric Thruster for Spacecraft with Mass up to 500 kg
- Purpose: Propulsion system of spacecraft by mass up to 500 kg.
- Year of release: 2004
- Guaranteed service life (years): 15 (GSO)
- Estimated production / delivery time (months): 12
- Flight qualification of the product: Yes
- Brief history of flight qualification: Flight testds on SC GSAT-9 (launched on 13.05.2017). Thruster was used by purpose.
Parameter | Value |
---|---|
Thrust, mN | 18 |
Power, kW | 0,35 |
Specific impulse, s | 1450 |
Mass, kg | 2 |
Designed service life, hours | > 3500 |
Electric propulsion. It has high efficiency at low power.
Legal information
Please note that this site is for informational purposes only and under no circumstances is not a public offer determined by the provisions of the Part 2 Article 437 of the Civil code of the Russian Federation.
Information on this site may be changed or supplemented.