A spacecraft includes payload equipment and bus equipment, each of the payload equipment and the bus equipment being coupled with a secondary structure arrangement. The spacecraft is configured to structurally interface with a launch vehicle upper stage only by way of an exoskeletal launch support structure (ELSS) that provides a first load path between a launch vehicle upper stage and the secondary structure arrangement. The spacecraft is configured to deploy from the launch vehicle upper stage by separating from the ELSS. In some implementations, the first load path is the only load path between the spacecraft and the launch vehicle upper stage, and substantially all of the ELSS remains with the launch vehicle upper stage. Because the secondary structure may be substantially less massy then the ELSS, subsequent orbit raising maneuvers may then be executed with a spacecraft having a reduced dry mass.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Exoskeletal launch support structure


    Beteiligte:
    CHIANG JASON (Autor:in)

    Erscheinungsdatum :

    2020-04-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    EXOSKELETAL LAUNCH SUPPORT STRUCTURE

    CHIANG JASON | Europäisches Patentamt | 2018

    Freier Zugriff

    Exoskeletal technology

    Vykukal, H. C. | NTRS | 1974



    Structural Evaluation of Exoskeletal Engine Fan Blades

    Chamis, C. / Kuguoglu, L. / Abumeri, G. et al. | British Library Conference Proceedings | 2003


    Structural Evaluation of Exoskeletal Engine Fan Blades

    Kuguoglu, Latife / Abumeri, Galib / Chamis, Christos | AIAA | 2003