Powered part of flight path of unguided rocket influenced by variable cross wind and thrust malalignment is calculated on digital computer; magnitude of deviation caused by distinct disturbances depends on aerodynamic data of missile; optimum yaw oscillation distance decreases with increasing frequency of cross wind.


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    Title :

    Influence of aerodynamic parameters on dispersion of unguided rockets due to gusts


    Additional title:

    AGARD Conference Proc


    Contributors:

    Conference:

    AGARD Conference ; 1966 Orbits and trajectories


    Published in:

    Publication date :

    1966


    Size :

    30 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English