Based on the public materials, this paper collects the overall parameters of SpaceX's super heavy starship launch vehicle, estimates some of the undisclosed parameters required for the calculation in order to meet the requirements of the simulation, and carries out the study of the optimal trajectory design method for the vertical return of the two-stage rocket on this basis, and completes the simulation of the super heavy starship rocket for a typical LEO launch mission.


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    Titel :

    Optimal launch capacity trajectory design for SpaceX's super heavy starship launch vehicle


    Beteiligte:
    Shao, Xiaopeng (Herausgeber:in) / Zhang, Xuemei (Autor:in)

    Kongress:

    Third International Computing Imaging Conference (CITA 2023) ; 2023 ; Sydney, Australia


    Erschienen in:

    Proc. SPIE ; 12921


    Erscheinungsdatum :

    06.11.2023





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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