A space vehicle includes: an aerospike nozzle formed on an aft end of the vehicle; a truncated spike including an outer edge and a surface formed on a rear portion of the truncated spike; and an annular ring outlet formed at the aft end of the vehicle between the outer edge of the truncated spike and an inner edge of the aft end of the space vehicle.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Reusable vertical take-off and landing space launch vehicle


    Beteiligte:

    Erscheinungsdatum :

    2020-09-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Landing apparatus for reusable launch vehicle

    JUNG DONG HO | Europäisches Patentamt | 2023

    Freier Zugriff

    Landing apparatus for reusable launch vehicle

    Europäisches Patentamt | 2023

    Freier Zugriff

    LANDING APPARATUS FOR A REUSABLE LAUNCH VEHICLE

    JUNG DONG HO | Europäisches Patentamt | 2023

    Freier Zugriff

    Landing apparatus for a reusable launch vehicle

    JUNG DONG HO | Europäisches Patentamt | 2023

    Freier Zugriff

    Dynamic analysis for vertical soft landing of reusable launch vehicle with landing strut flexibility

    Yue, Shuai / Nie, Hong / Zhang, Ming et al. | SAGE Publications | 2019