Electric Thruster for Spacecraft with Mass up to 500 kg

    • Electric Thruster for Spacecraft with Mass up to 500 kg

    Purpose:
    Propulsion system of spacecraft 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.
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    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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