Review of jet hydraulic system data indicated that two-thirds of all hydraulic system incidents during past 2 yr have been due to external system leakage in areas of lines, fittings, hoses, and seals; these areas must be given extensive consideration in design of SST; preliminary studies indicate that approximately 700 hydraulic hp may be used for various hydraulic systems; this might include 250 hp for flight control system; it is anticipated that hydraulic system operational temperatures will vary from 350 to 500 F.


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    Title :

    Supersonic transport aircraft hydraulic systems


    Additional title:

    J Aircraft


    Contributors:

    Published in:

    Publication date :

    1964


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    Supersonic Transport Aircraft

    Emerald Group Publishing | 1961


    Supersonic transport aircraft

    Russell, A.E. | Engineering Index Backfile | 1962


    Supersonic transport aircraft

    Engineering Index Backfile | 1961