Destruction ground tests have been carried out using three scaled down solid propellant motors using pairs of V-shaped charges. Each motor is a one/tenth scale model of the first stage of the Mu-3C, an all solid propellant satellite launcher developed by ISAS. Destruction devices in these tests are roughly the same in function and installation as those for the Mu-3C. Several interesting results have been obtained on the breakup characteristics of the motor, such as mode of destruction, shapes of fragments of propellant and hardware, scattering distribution, the shock load undergone by the motor and the ambient overpressure. These results are expected to be useful for the prediction of the breakup characteristics of the Mu-3C during destruction in flight by the V-shaped charges.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Destruction Test of Small Scaled Solid Propellant Motors


    Beteiligte:
    M. Hinada (Autor:in) / R. Akiba (Autor:in) / T. Kishi (Autor:in) / Y. Matogawa (Autor:in) / S. Tsukamoto (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Solid propellant rocket motors

    Maxwell, W.R. / Young, G.H.S. | Engineering Index Backfile | 1961


    Large solid-propellant motors

    Crook, J.H. | Engineering Index Backfile | 1960