A thrust stand and calibration system is described by which the direction of the thrust vector of a rocket motor can be resolved over consecutive 50 msec intervals to within 0.7 milliradian. The angle of the overall impulse vector can be measured to better than 0.5 milliradian. Methods of improving the accuracy of the system are discussed. (Author)


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    Titel :

    The Design of a Stand to Measure Thrust Alignment in Solid Propellent Rocket Motors


    Beteiligte:
    D. S. Dean (Autor:in) / E. A. Lyons (Autor:in) / D. R. Norman (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    29 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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