This paper concerns a new technique designed to provide high performance reaction control systems for sounding rockets. Proportional control of differential thrust and simple adaptive control of thrust magnitude (based on the level of demanded thrust) is utilized. The control is being implemented with a combination of electronic and fluidic components for an Aerobee 150 sounding rocket payload whose goal is a pointing stability of 0.1 arc second.


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    Titel :

    A New Reaction Control Approach for Sounding Rockets


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Gabris, E. A. (Autor:in) / Murphy, J. P. (Autor:in) / Honda, T. S. (Autor:in) / Keltz, W. L. (Autor:in)

    Kongress:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1970



    Erscheinungsdatum :

    1970-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    A new reaction control approach for sounding rockets

    Gabris, E. A. / Honda, T. S. / Keltz, W. L. et al. | NTRS | 1970


    Sounding Rockets

    Newell, Homer Edward | GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1959


    Sounding rockets

    Pressly, E. C. | NTRS | 1965


    Sounding Rockets

    Newell, Homer Edward | TIBKAT | 1959


    French sounding rockets

    Sournia, F. | Engineering Index Backfile | 1964