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.


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    Title :

    Shuttle Orbiter arrestment system studies


    Contributors:

    Publication date :

    1988-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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