The actuation system for the Saturn V S-IC stage is described and compared to the Saturn I system. The use of mechanical feedback actuators that result in a significant increase in system reliability and the damping of load resonance is discussed. The unprecedented component sizes and system requirements are cited.The components of the S-IC stage engine gimbal actuation system are similar to and a direct evolution of those used in the Saturn I vehicle system.The major system components are the fluid supply, a filter manifold, lines, and the actuators. The system is the essence of simplicity. As a fluid power source, fuel is taken directly in a single path from the high pressure side of the engine turbopump. Flow from the actuators is returned to the fuel system rather than to a reservoir.Because of the small number of components and the design concepts used, the reliability of this system is high.


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    Titel :

    Saturn V S-IC Stage Engine Gimbal Actuation System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Kalange, M. A. (Autor:in) / Alcott, R. J. (Autor:in)

    Kongress:

    Aerospace Fluid Power Systems and Equipment Conference ; 1965



    Erscheinungsdatum :

    1965-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Saturn v s-ic stage engine gimbal actuation system.

    Alcott, R. J. / Kalange, M. A. | NTRS | 1965


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    Jacobs, M. R. / McGillen, V. W. | SAE Technical Papers | 1965