Equations obtained for calculating divergence speed of multistage rocket; analysis assumes that total lift separates into components working on several points of rocket body and that inertial force of body is equated with separated lifts; aerodynamic characteristics values necessary to calculate divergence speed can be obtained by wind tunnel test of model and simple bending test of body.


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    Titel :

    Body divergence of multi-stage rocket


    Weitere Titelangaben:

    Tokyo. Univ -- Inst Space Aeronautical Science -- Report


    Beteiligte:
    Ikeda, K. (Autor:in) / Hirano, Y. (Autor:in)


    Erscheinungsdatum :

    1967


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Body Divergence of a Multi-Stage Rocket

    Y. Hirano / K. Ikeda | NTIS | 1967


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