High-powered Electric Thruster for Spacecraft with Mass up to 3000 kg

Purpose:
Propulsion system of spacecrafts by mass up to 3000 kg.
Year of release: 2001
Guaranteed service life (years): 15 (GSO)
Estimated production / delivery time (months): 12
Flight qualification of the product: No
Brief history of flight qualification:
Qualification model.
Possibility to adapt the product to customer requirements: Yes


Parameter Value
Thrust, mN 200 / 380
Power, kW 3,5 / 6,0
Specific impulse, s 1700 / 2650
Mass, kg 8
Designed service life, hours > 6000

Description

Electric propulsion. Multimode thruster. Cathodes on the basis of W-Ba emitter.

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