Electric Thruster for Spacecraft with Mass up to 3000 kg

Purpose:
Propulsion system of spacecrafts by mass up to 3000 kg.
Year of release: 2011
Guaranteed service life (years): 15 (GSO)
Estimated production / delivery time (months): 12
Flight qualification of the product: No
Brief history of flight qualification:
Flight set was delivered to the customer.
Possibility to adapt the product to customer requirements: Yes


Parameter Value
Thrust, mN 72
Power, kW 1,65
Specific impulse, s 2680
Mass, kg 6
Designed service life, hours > 4000

Description

Electric propulsion. High specific impulse. Cathodes on the basis of W-Ba emitter.

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