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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    Title :

    Analysis of toroidal actuation systems for aerospace vehicles


    Additional title:

    SAE-NASA -- Proc


    Contributors:
    Dreher, H. (author)

    Conference:

    Proceedings of the Aerospace Vehicle Flight Control Conference ; 1965 Control


    Published in:

    Publication date :

    1965


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :