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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Body divergence of multi-stage rocket


    Additional title:

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


    Contributors:
    Ikeda, K. (author) / Hirano, Y. (author)


    Publication date :

    1967


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Body Divergence of a Multi-Stage Rocket

    Y. Hirano / K. Ikeda | NTIS | 1967


    MULTI-STAGE ROCKET

    SUDA HIROSHI | European Patent Office | 2021

    Free access

    On Simplified Mechanical Models for Rocket-Body Divergence and Flutter

    Ohshima, Tsukasa / Sugiyama, Yoshihiko | AIAA | 2003


    On Simplified Mechanical Models for Rocket-Body Divergence and Flutter

    Ohshima, T. / Sugiyama, Y. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003


    MULTI STAGE TOY ROCKET

    European Patent Office | 2020

    Free access