Stationary Plasma Thruster with a Discharge Power of up to 6 kW

    • Stationary Plasma Thruster with a Discharge Power of up to 6 kW

    Purpose:
    Spacecraft station keeping. Spacecraft orbit raising to GEO
    Year of release: 2015
    Guaranteed service life (years):
    35000 hours 7000 cycles
    Estimated production / delivery time (months): 12
    Flight qualification of the product: No
    Brief history of flight qualification: None
    Possibility to adapt the product to customer requirements: Yes
    Submit application


    Parameter Value
    Discharge power 4500/6000 W
    Discharge voltage 300/600 V
    Discharge current 15.0/10.0 A
    Thrust 290/250 mN
    Specific impulse 1850/2400 s
    Efficiency 60%
    Specific power 555/741 W/kg
    Power-to-thrust ratio 15.5/24 W/mN
    Total impulse > 20 MN∙s
    Mass 8.1 kg

    Description

    Thruster with a discharge power of up to 6 kW. Propellant - xenon. Development status – laboratory model. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens. Outside diameter of the accelerating
    ... Thruster with a discharge power of up to 6 kW.
    Propellant - xenon.
    Development status – laboratory model.
    Consists of the anode and cathode units.
    Classical scheme of the magnetic system with magnetic screens.
    Outside diameter of the accelerating channel is 140 mm. Mean diameter of the accelerating channel is 120 mm.
    New structural materials and components
    Read more...

    Remark

    Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months).

    Legal information
    Please note that this site is for informational purposes only and under no circumstances is not a public offer determined by the provisions of the Part 2 Article 437 of the Civil code of the Russian Federation. Information on this site may be changed or supplemented.