Attitude Control Propulsion Unit

    • Attitude Control Propulsion Unit

    Purpose:
    Creating steering effort in the attitude modes and in the spacecraft survivability modes.
    Year of release: 2003
    Guaranteed service life (years): 19
    Estimated production / delivery time (months): 7
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    Parameter Value
    Operating propellant Xenon (State Standard GOST 10219-77)
    Nominal nozzle thrust, N (gf) 7.85×10-2 (8)
    Active lifetime, years 15.5
    Mass, kg, not exceeding 0.33

    Description

    Pneumatic automation equipment.

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