Evolution of attitude control systems related to NASA space vehicles is covered; successful employment of electric thrust vector control on Mercury-Redstone was followed by employment of fluid power for Juno II, Saturn, and advanced Saturn; comparison made of electric and hydraulic systems as exemplified by Pershing and Mercury-Redstone; other applications of fluid power related to space vehicles; advantages of fluid power.


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    Titel :

    Technical advantages of fluid power


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Neiland, V.R. (Autor:in) / Kalange, M.A. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Hydraulic equipment



    Erscheinungsdatum :

    1962


    Format / Umfang :

    39 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    TECHNICAL ADVANTAGES OF FLUID POWER

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    Technical Advantages Of Fluid Power

    KALANGE, M. A. / NEILAND, V. R. | SAE Technical Papers | 1962


    The technical advantages of IFTE over its predecessors

    Ucci, R.M. / Romania, J.J. jun. | Tema Archiv | 1987


    Technical and Economic Advantages Offered by Multicomponent Blends

    Lee, R. / Wu, M. / Zenner, J. et al. | British Library Conference Proceedings | 1999


    Large LNG carrier poses economic advantages, technical challenges

    Cho, Joseph H. / Kotzot, Heinz / Vega, Felix de la et al. | Tema Archiv | 2005