Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XFC Unit)

    • Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XFC Unit)

    Purpose:
    Spacecraft (S/C) station keeping
    Year of release: 2001
    Guaranteed service life (years):
    4500 hours 3000 cycles
    Estimated production / delivery time (months): 12
    Flight qualification of the product: Yes
    Brief history of flight qualification:
    As part of: S/C of Cosmos series; S/C of Luch series (launched on 16.12.94, 11.10.95); Kupon S/C (launched on 16.12.94); S/C of Yamal series (launched on 06.09.99, 24.12.03); KazSat-1 (launched on 18.06.06); KazSat-2 (launched on 16.07.11); Express-MD1 (launched on 11.02.09): Express-MD2 (launched on 06.08.12); EgiptSat-F (launched 22.02.19))
    Possibility to adapt the product to customer requirements: Yes
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    Parameter Value
    Discharge power 669 W
    Discharge voltage 300 V
    Discharge current 2.23 A
    Thrust 39 мН
    Specific impulse 1470 s
    Efficiency 43%
    Specific power 238 W/kg
    Power-to-thrust ratio 17.2 W/mN
    Total impulse > 0.5 MN∙s
    Mass 2.8 kg

    Description

    Consists of two units: M-70 Stationary Plasma Thruster and Xenon Flow Controller Unit (XFC Unit). Propellant - xenon.

    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).

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