FIELD: rocket technology.SUBSTANCE: invention relates to the field of rocket technology, and more specifically to the separation system. The rocket compartment separation unit includes power attachment units for the frames of the separated compartments, pyrolysis units for the power attachment units’ lock release and the compartment pusher. The pyrolysis unit for the power attachment units’ lock release is installed in a movable flange and is made in the form of a pneumatic cylinder with a piston that is shifted relative to the movable flange and the frame with a pusher of the compartment made on it. The pusher of the compartment passes through a cutout made in the frame, with an emphasis on the frame of another of the separated compartments.EFFECT: increased reliability of the flyer is achieved.1 cl, 6 dwg

    Изобретение относится к области ракетной техники, а более конкретно к системе разделения. Узел разделения отсеков ракеты включает силовые узлы крепления шпангоутов разделяемых отсеков, пироузлы расфиксации силовых узлов крепления и толкатель отделения. Пироузел расфиксации силовых узлов крепления установлен в подвижный фланец и выполнен в виде пневмоцилиндра со сдвигаемым относительно подвижного фланца и шпангоута поршнем с выполненным на нем толкателем отделения. Толкатель отделения проходит через вырез, выполненный в шпангоуте, с упором на шпангоут другого из разделяемых отсеков. Достигается повышение надежности летательного аппарата. 6 ил.


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    Title :

    ROCKET COMPARTMENT SEPARATION UNIT


    Additional title:

    Узел разделения отсеков ракеты


    Contributors:

    Publication date :

    2021-09-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



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