• DocumentCode
    2336381
  • Title

    Horizontal stabilization of a rocket launcher transporter

  • Author

    Ota, Y. ; Mizunuma, W. ; Konuma, H. ; Nohara, B.T.

  • Author_Institution
    Iwatsuka Nakamura-ku, Nagoya, Japan
  • fYear
    2000
  • fDate
    1-1 April 2000
  • Firstpage
    351
  • Lastpage
    355
  • Abstract
    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.
  • Keywords
    hydraulic systems; pressure control; rockets; stability; transportation; vibration control; H-II rocket; active suspension; horizontal stabilization system; hydraulic system; pressure control; rocket launcher transporter;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Motion Control, 2000. Proceedings. 6th International Workshop on
  • Conference_Location
    Nagoya, Japan
  • Print_ISBN
    0-7803-5976-3
  • Type

    conf

  • DOI
    10.1109/AMC.2000.862890
  • Filename
    862890