Electric Thruster for Spacecraft with Mass up to 500 kg

Purpose:
Propulsion system of spacecrafts 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

Description

Electric propulsion. It has high efficiency at low power.

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