By analyzing the shipboard missile vertical launching system (VLS), we simplified the assembly model and reconstructed it with mathematical methods, established the clearance parameter and deviation angle mathematical formulas. In considering of the assembly errors of guide rail in missile vertical launcher system, we studied assembly clearance parameters effects on the system at first. And then established dynamic simulation model, researched the relationship between assembly clearance parameters and missile launching status. At last, used the above relationship model and conclusions, developed a prototype simulation method, and provided the foundation and guidance for design of missile vertical launching system.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Analysis of Geometric Characteristic of Missile Vertical Launching System Guide Rail



    Erschienen in:

    Erscheinungsdatum :

    2014-08-18


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    VERTICAL AIR MISSILE LAUNCHING METHOD

    DORONIN VIKTOR VALENTINOVICH / SOKOLOVSKIJ VIKTOR VLADIMIROVICH / SAMONOV VIKTOR ALEKSEEVICH et al. | Europäisches Patentamt | 2020

    Freier Zugriff


    Missile Launching System

    S. Landstrom / R. E. Carlberg | NTIS | 1965


    Missile Launching Assembly

    R. W. Villers | NTIS | 1964


    Missile Launching Apparatus

    M. Chevillon | NTIS | 1964