The methodologies and development of the loads experienced during liftoff of the NASA SLS Block I vehicle will be presented in this paper. The liftoff loads analysis traditionally captures the dynamics of vehicle/pad separation after engine/booster ignition coupled with other launch day environments like wind, overpressure, and engine side loads. Additionally, the liftoff analysis includes an on-pad engine shutdown prior to booster ignition. The SLS liftoff analysis is performed using a Monte Carlo analysis and this paper will explore the Monte Carlo process and the statistical approach to calculating the limit loads.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Methodology and Development of SLS Liftoff Loads


    Beteiligte:
    David Alldredge (Autor:in) / Ben Jones (Autor:in) / Ty Irwin (Autor:in) / Skylar Taggart (Autor:in) / Austin F Decker (Autor:in)

    Kongress:

    AIAA SciTech Forum ; 2022 ; San Diego, CA, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Methodology and Development of SLS Liftoff Loads

    David Alldredge / Ben Jones / Austin Decker et al. | NTRS


    Methodology and Development of SLS Liftoff Loads

    Alldredge, David / Jones, Ben / Irwin, Ty et al. | AIAA | 2022



    Methodology and Development of SLS Liftoff Loads

    Alldredge, David / Jones, Ben / Irwin, Ty et al. | TIBKAT | 2022