A method is described whereby a rocket motor impulse lasting a few milliseconds may be spread over a longer period to allow it to be recorded by conventional methods with an accuracy of plus/minus 0.2%. Instantaneous thrust is also recorded with an accuracy of plus/minus 2%. Most of the problems encountered with a ballistic pendulum are avoided and only the static calibration of a load cell is required before use. (Author)


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    Titel :

    A Ballistic Technique for Accurate Measurement of Total Impulse and Thrust of Rocket Motors with Short Burning Times


    Beteiligte:
    D. S. Dean (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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