The dynamic stability and wind weighting problems of a spinning sounding rocket are investigated by numerical solution of the six equations of rigid body motion. Transition through the roll resonance regime is discussed, and first-stage trajectory dispersions are compared with those actually measured in flight on five vehicles. (Author)


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    Titel :

    Ascent Problems of Sounding Rockets


    Beteiligte:
    N. L. Crabill (Autor:in)

    Erscheinungsdatum :

    1961


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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