The requirements of hydraulic power units for the Supersonic Transport are compared with those for present commercial aircraft and with the requirements that have been met in supersonic military applications Trends in component power, speed, flow and other parameters, and their effects on component design are discussed.


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    Title :

    Hydraulic Power Units for Supersonic Aircraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Systems Conference and Engineering Display ; 1967



    Publication date :

    1967-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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