Scale model studies of the Shuttle Orbiter arrestment system were conducted to determine the proper net arrestment system configuration to bring the Orbiter to a safe stop in the event of a runway overshoot. Areas of interest include the effect of various net geometries on net engagement of the nose gear and main gear; and whether or not the top bundle contacts the crew cabin window. The model tests indicated that the net arrestment system was properly designed to bring the Orbiter to a safe stop with minimal amount of damage. The test procedures and data are presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Shuttle Orbiter arrestment system studies


    Beteiligte:

    Erscheinungsdatum :

    01.10.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Shuttle Orbiter Arrestment System Studies

    Davis, Pamela A. / Stubbs, Sandy M. | SAE Technical Papers | 1988


    Studies of Shuttle Orbiter Arrestment System

    P. A. Davis / S. M. Stubbs | NTIS | 1993


    Studies of Shuttle orbiter arrestment system

    Davis, Pamela A. / Stubbs, Sandy M. | NTRS | 1993


    Arrestment System

    K. T. Koper | NTIS | 1980


    Arrestment System

    K. T. Koper | NTIS | 1979