Scale model studies of the Shuttle Orbiter Arrestment System (AS) were completed with a 1/27.5-scale model at the NASA Langley Research Center. The purpose of these studies was to determine the proper configuration for a net arrestment system to bring the orbiter to a safe stop with minimal damage in the event of a runway overrun. Tests were conducted for runway on-centerline and off-centerline engagements at simulated speeds up to approximately 100 knots (full scale). The results of these tests defined the interaction of the net and the orbiter, the dynamics of off-centerline engagements, and the maximum number of vertical net straps that may become entangled with the nose gear. In addition to these tests, a test program with a 1/8-scale model was conducted by the arrestment system contractor, and the results are presented in the appendix.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Studies of Shuttle orbiter arrestment system


    Contributors:

    Publication date :

    1993-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Shuttle Orbiter arrestment system studies

    Davis, Pamela A. / Stubbs, Sandy M. | NTRS | 1988


    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


    Arrestment System

    K. T. Koper | NTIS | 1980


    Arrestment System

    K. T. Koper | NTIS | 1979