THE S-3A VEHICLE is equipped with 2 completely independent hydraulic systems which have been designated as the combined flight control/utility system. These systems are both structurally and hydraulically isolated from each other and are designed and installed in accordance with spec. MIL-H-5440 type II (−65° to 275°F temperature range) class 3000 (cutout pressure at pump is 3,100psi).


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    Title :

    Combined flight control/utility system



    Publication date :

    1974-03-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English