Spacecraft Separation Device

    • Spacecraft Separation Device

    Purpose:
    Spacecraft attachment to the adapter for the period of their joint operation; shock-free separation of the spacecraft with the specified parameters using the command from the booster control unit.
    Year of release: 2011
    Guaranteed service life (years): 6
    Estimated production / delivery time (months): 12
    Brief history of flight qualification:
    Amos-5, Yamal-300K, Express-АТ1, Express-АТ2, Express-АМ8, KazSat-3, Loutch-5V, Express-АМ5, Express-АМ6, Yamal-401.
    Submit application


    Parameter Value
    Separation device mass, kg 10.5 to 15
    Attitude rate of spacecraft separation no greater than 3% relative to any axis
    Linear velocity of spacecraft separation, m/s 1.5±0.5
    Separating spacecraft mass, kg 1600 to 3400
    Number of locks, units 6 or 12
    Maximum permissible axial equivalent force at the separation interface up to 1080000 N
    Number of push-rod springs 6 or 8

    Description

    Mechanical device that consists of locks, spring-loaded pushrods, clamp-band with explosive pins, separation connectors, separation sensors.

    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.