Approach taken by Lycoming-Stratford Div, Avco Corp, in development of mechanical servo actuator for all-mechanical flight control system for advanced supersonic aircraft and space vehicles; description of actuator and its basic design criteria; component and system test results, including parametric and theoretical analyses, substantiate feasibility of approach; techniques for tailoring performance to specific requirement and approach to mechanical cascading for control power amplification are considered. SAE-Paper 650580.


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    Titel :

    Analysis of toroidal actuation systems for aerospace vehicles


    Weitere Titelangaben:

    SAE-NASA -- Proc


    Beteiligte:
    Dreher, H. (Autor:in)

    Kongress:

    Proceedings of the Aerospace Vehicle Flight Control Conference ; 1965 Control


    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :