The staging mechanisms of the Japanese satellite launch vehicle Mu-3SII involving a unique separation and jettison mechanism for the nose fairing are described. The design requirements, the design features and the development problems are presented together with their solutions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The Development of Staging Mechanisms for the Japanese Satellite Launcher Mu-3SII


    Contributors:
    Onoda, J. (author)


    Publication date :

    1985-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Launcher Staging

    Cerf, Max | Wiley | 2024


    Minimum-cost satellite launcher

    Godwin, F. | Engineering Index Backfile | 1965


    DSI Small Satellite Launcher

    S. Nichols / D. Gibbons / J. Wise et al. | NTIS | 1992


    Ariane: Europe's satellite launcher

    Dance, B. | Tema Archive | 1979


    SATELLITE LAUNCHER AND METHOD FOR PUTTING SATELLITES INTO ORBIT USING SAID SATELLITE LAUNCHER

    LÓPEZ-URDIALES JOSÉ MARIANO | European Patent Office | 2018

    Free access