The Launcher Stabilization System (LSS) is a pneumatic/hydraulic ground system used to support an Atlas launch vehicle prior to launch. The redesign and development activity undertaken to achieve an LSS with increased load capacity and a redundant hydraulic system for the Atlas 2 launch vehicle are described.


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    Title :

    Design and Development of the Redundant Launcher Stabilization System for the Atlas 2 Launch Vehicle


    Contributors:
    M. Nakamura (author)

    Publication date :

    1991


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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