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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:
    Onoda, J. (Autor:in)


    Erscheinungsdatum :

    01.08.1985


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    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 Archiv | 1979


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

    LÓPEZ-URDIALES JOSÉ MARIANO | Europäisches Patentamt | 2018

    Freier Zugriff