A spacecraft may include an upper core structure (148) or a lower core structure (168). The upper core structure (148) may include an upper cylinder (150) for supporting an upper spacecraft (146) of a dual-manifest launch configuration. The lower core structure (168) may include a lower cylinder (170) for supporting a lower spacecraft (166) with the upper cylinder (150) mounted on top of the lower cylinder (170). The upper cylinder (150) may have an upper cylinder inner diameter that may be substantially similar to the lower cylinder inner diameter.


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    Titel :

    Modular core structure for dual-manifest spacecraft launch


    Weitere Titelangaben:

    Modulare Kernstruktur für Rakete mit zwei Nutzlasten
    Structure de noyau modulaire pour lanceur à deux charges utiles


    Beteiligte:
    ASTON RICHARD (Autor:in) / TOMZYNSKA ANNA (Autor:in) / LANGMACK MICHAEL (Autor:in) / PETERKA JAMES (Autor:in)

    Erscheinungsdatum :

    11.04.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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