The invention relates to aerospace engineering and may be used in designing spacecrafts of middle class for various purposes. The proposed method allows unifying the payload module at the lowest cost, along with simplifying the design of the module. The invention provides optimal mass and weight characteristics, as well as high assemblability. The objective is to create a new assembly unit that has less weight, high accuracy, along with increased reliability and maximum simplification of the assembling process. The technical result of the invention is in determining the sequence of installation of elements of the load-bearing structure of payload module, with combined use of composite materials and metals, ease of installation and assembly of the structure, which allows optimizing the phasing, assembly time, and also increasing reliability of the created spacecrafts.


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    Titel :

    СПОСОБ СБОРКИ КОСМИЧЕСКОГО АППАРАТА


    Erscheinungsdatum :

    2017-10-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS