The evaluation program consisted of F-4 Flight Control Simulator (Iron Bird) hydraulic systems tests and tests in selected separate subsystems. The F4 Flight Control Simulator tests included a dynamic performance comparison between MLO-68-5 and MIL-H-5606, and an endurance test was conducted by cycling through three typical mission profiles. Separate tests were conducted using the F-4 utility system suction line subsystem, aerial refueling subsystem, and arresting gear subsystem. Fluid characteristics, including flash point, viscosity, etc., were checked periodically in all tests. In addition, a 'drain and fill' procedure for converting from MIL-H-5606 to MLO-68-5 without the use of an intermediate fluid was developed. (Author)


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    Title :

    Evaluation of MLO-68-5 Less Flammable Hydraulic Fluid


    Contributors:
    J. L. Herr (author) / N. J. Pierce (author)

    Publication date :

    1970


    Size :

    170 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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