The braking system for a short takeoff aircraft is discussed and the deficiencies are described. The installation of a Boeing 727 aircraft brake system was made to correct the deficiencies. Tests of the modified system were conducted using an analog computer/hardware simulator. Actual performance tests were conducted and the characteristics of the system were satisfactory.


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    Title :

    Brake control system modification, augmentor Wing Jet STOL Research Airplane (AWJSRA)


    Contributors:

    Publication date :

    1974-06-24


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :