TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster

    • TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster

    Purpose:
    Spacecraft orientation and attitude control.
    Year of release: 2013
    Guaranteed service life (years): 5
    Estimated production / delivery time (months): 12
    Flight qualification of the product: Yes
    Possibility to adapt the product to customer requirements: Yes
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    Parameter Value
    Heater unit power consumption 7.3 W
    Overall dimensions 171х58х109 mm
    Mass 0.59 kg

    Description

    Propellant - hydrazine. The unit consists of one modified thermocatalytic low thruster. Thermal mode of the unit is ensured by 2 heaters (1 main and 1 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 3 temperature sensors.

    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
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