Electric Thruster for Spacecraft with Mass up to 2500-3000 kg

Purpose:
Propulsion system of spacecrafts by mass up to 2500 - 3000 kg.
Year of release: 2018
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 95
Power, kW < 2,4
Specific impulse, s 2680
Mass, kg 5,25
Designed service life, hours > 6000

Description

Electric propulsion. Record specific impulse and propulsion resource for Hall-effect thrusters.

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