A newly designed rocket launcher transporter is developed for transporting the post H-II rocket. The rocket is transported by two transporters electrically and hydraulically attached to each other. This paper focuses on the horizontal stabilization system. The total weight of a rocket and its holder is 1,265 ton, so that the active suspension is worked by the hydraulic system. The transporter has a 56 multi-wheel drive system and the active suspension is used to stabilize horizontally the rocket holder and the rocket itself by hydraulic pressure control on each wheel. Even on a bumpy road, the performance of /spl plusmn/0.2 degree or less in the horizontal stabilization was achieved.


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    Titel :

    Horizontal stabilization of a rocket launcher transporter


    Beteiligte:
    Ota, Y. (Autor:in) / Mizunuma, W. (Autor:in) / Konuma, H. (Autor:in) / Nohara, B.T. (Autor:in)


    Erscheinungsdatum :

    2000-01-01


    Format / Umfang :

    562009 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Horizontal Stabilization of a Rocket Launcher Transporter

    Ota, Y. / Mizunuma, W. / Konuma, H. et al. | British Library Conference Proceedings | 2000


    Rocket Launcher

    B. M. Jones / R. H. Forster / G. L. West et al. | NTIS | 1968


    Transporter launcher

    MORTON GUY STEWART / WEBB MILES LEONARD DAVID | Europäisches Patentamt | 2016

    Freier Zugriff

    Rocket Launcher Studies

    D. Rossin / P. R. Zagala / V. J. Taylor et al. | NTIS | 1964


    Supersonic Rocket Launcher

    E. P. Lowe / R. D. Stubbs | NTIS | 1975