NASA's new Space Launch System (SLS) will be the first rocket since the Saturn V (1967-1973) to carry astronauts beyond low earth orbit-and will carry 10% more payload than Saturn V and three times the payload of the space shuttle. The SLS configuration consists of a center core and two solid rocket boosters that separate from the core as their fuel is exhausted two minutes after lift-off. During these first two minutes of flight, the vehicle powers its way through strong shock waves as it accelerates past the speed of sound, then pushes beyond strong aerodynamic loads at the maximum dynamic pressure, and is ultimately enveloped by gaseous plumes from the booster-separation motors. The SLS program relies on computational fluid dynamic (CFD) simulations to provide much of the data needed to build aerodynamic databases describing the structural load distribution, surface pressures, and aerodynamic forces on the vehicle.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Building Aerodynamic Databases for the SLS Design Process


    Beteiligte:
    Rogers, Stuart (Autor:in) / Dalle, Derek J. (Autor:in) / Lee, Henry (Autor:in) / Meeroff, Jamie (Autor:in) / Onufer, Jeffrey (Autor:in) / Chan, William (Autor:in) / Pulliam, Thomas (Autor:in)

    Kongress:

    Supercomputing 2017 ; 2017 ; Denver, CO, United States


    Erscheinungsdatum :

    2017-11-12


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aerodynamic Databases

    Abzug, Malcolm J. | AIAA | 1998


    Building Aerodynamic Databases for the Space Launch System

    Jamie Meeroff / Stuart Rogers / Derek Dalle et al. | NTRS


    Building Booster Separation Aerodynamic Databases for Artemis II

    Meeroff, Jamie G. / Dalle, Derek J. / Rogers, Stuart E. et al. | NTRS | 2019


    Building Aerodynamic Databases for the Space Launch System

    J. Meeroff / S. Rogers / D. Dalle et al. | NTIS | 2022