Technology is disclosed herein for a spacecraft launch restraint and dispensing structure. The dispensing structure has a number of trusses and a central structure. When the trusses are in a support position, each spacecraft may be supported at one point by the central structure and at two points by one or more of the trusses. Therefore, each spacecraft may be supported at three points, thereby providing a stable support for each spacecraft. The spacecrafts do not touch each other and do not bear the weight of other spacecrafts. In a deployment position, the trusses extend away from the satellites and do not support the satellites; however, the satellites initially remain connected to the central structure. In the deployment position, the trusses are out of an ejection path such that the satellites can be ejected in a desired sequence from the central structure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    MULTI-SATELLITE DEPLOYABLE DISPENSER


    Beteiligte:

    Erscheinungsdatum :

    2023-03-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    MULTI-SATELLITE DEPLOYABLE DISPENSER

    BAGHDASARIAN VAROUJ | Europäisches Patentamt | 2024

    Freier Zugriff

    Multi-satellite deployable dispenser

    BAGHDASARIAN VAROUJ | Europäisches Patentamt | 2023

    Freier Zugriff

    MULTI-SATELLITE DEPLOYABLE DISPENSER

    BAGHDASARIAN VAROUJ | Europäisches Patentamt | 2023

    Freier Zugriff

    Deployable satellite mast

    VILLEMAIN ALEXIS | Europäisches Patentamt | 2023

    Freier Zugriff

    DEPLOYABLE SATELLITE MAST

    VILLEMAIN ALEXIS | Europäisches Patentamt | 2020

    Freier Zugriff