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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    Titel :

    Design and development of the redundant launcher stabilization system for the Atlas 2 launch vehicle


    Beteiligte:
    Nakamura, M. (Autor:in)


    Erscheinungsdatum :

    01.05.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





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