General equations of motion are derived for spinning elastic rocket with respect to axes attached to rocket; equations contain force and moment system that includes, in addition to usual quasisteady forces and moments, those due to Magnus effects; as result, stability criteria for spinning elastic rocket are approximately derived, including those for case of rigid body and for case of nonspinning elastic rocket, which have been analyzed; comparing analytical results with digital computational results, applicability of stability criteria is examined and empirical formulas for stability boundaries are presented.


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    Titel :

    On dynamic stability of rockets


    Weitere Titelangaben:

    Tokyo Univ -- Aeronautical Research Inst -- Report


    Beteiligte:
    Tomita, B. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    34 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Dynamic Stability Study for Sounding Rockets Final Report

    D. A. Price / P. S. Woods | NTIS | 1968


    Dynamic stability study for sounding rockets Final report

    Price, D. A., Jr. / Woods, P. S. | NTRS | 1968