Task I encompassed the design, development and procurement of hardware, sensors, and microprocessors for two diagnostic monitoring systems. The first system was installed on the F-14 Hydraulic Flight Simulator on Task II of the program. Task II included the installation of one system on the F-14A Hydraulic Simulator for system component reliability demonstrations. The task also covered simulated component failures and diagnostic system reaction. In Task III, the Diagnostic System was integrated into A6E B/N 155628. The System was debugged and a 12 month flight test schedule. This report covers Task III. (DePo)


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    Title :

    Hydraulic diagnostic monitoring system


    Additional title:

    Hydraulisches Diagnosis- und Ueberwachungssystem fuer Flugzeuge


    Contributors:

    Published in:

    Publication date :

    1981


    Size :

    303 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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