New MIL-E-5272 specification covers various tests conditions including temperatures from -85 F to 185 F, altitudes from sea level to 85,000 ft, humidity to 100%, exposure to salt sea atmosphere, vibration, etc; application to testing particular units; design for test chamber suggested that could simulate all of various weather conditions set forth in new directives.


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    Title :

    Environmental testing of aircraft hydraulic systems


    Additional title:

    Applied Hydraulics


    Contributors:

    Published in:

    Publication date :

    1951


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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