Electric Thruster for Spacecraft with Mass up to 1500 kg

Purpose:
Propulsion system of spacecrafts by mass up to 1500 kg.
Year of release: 2012
Guaranteed service life (years): 15 (GSO)
Estimated production / delivery time (months): 12
Flight qualification of the product: Yes
Brief history of flight qualification:
Operated as part of the motor subsystem correction since 2014.
Possibility to adapt the product to customer requirements: Yes


Parameter Value
Thrust, mN 42
Power, kW < 0,93
Specific impulse, s 1860
Mass, kg 3,1
Designed service life, hours > 4000

Description

Electric propulsion. It has high specific impulse at relatively low power. The record number of burnings is up to 20000 cycles.

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