The technique of launching aerodynamic models at hypersonic speeds with a helium-operated, heavy-piston-type, two-stage, light-gas launcher is discussed. The theoretical design of a launcher to give constant acceleration to the model is presented. A computer study for predicting the launcher performance is conducted using a one-dimensional hydrodynamics computer code. The performance of the launcher is studied experimentally, and the optimization is investigated. (Author)


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    Titel :

    Studies on Hypervelocity Model Launcher


    Beteiligte:
    G. Kamimoto (Autor:in) / A. Tsukamoto (Autor:in) / K. Otsuji (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    63 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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