The invention relates to a system (10) for separating composites of a space launch vehicle, comprising non-pyrotechnic separating modules (12) distributed between the composites to be separated and a device (14) for activating the separation modules (12), which can generate the simultaneous activation of all of the separating modules (12), characterised in that the activation device (14) consists of a source of compressed gas, the outlet of which is connected to each separation module (12).

    L'invention concerne un système de séparation (10) de composites d'un lanceur spatial comportant des modules de séparation non pyrotechniques (12) répartis entre les composites à séparer et un dispositif d'activation (14) des modules de séparation (12) qui est apte à provoquer l'activation simultanée de tous les modules de séparation (12), caractérisé en ce que le dispositif d'activation (14) consiste en une source de gaz comprimé dont la sortie est reliée à chaque module de séparation (12).


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    Title :

    MULTIPOINT SEPARATION SYSTEM


    Additional title:

    SYSTEME DE SEPARATION MULTIPOINTS


    Contributors:

    Publication date :

    2019-06-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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