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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    Titel :

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


    Beteiligte:
    Amberg, R. L. (Autor:in) / Arline, J. A. (Autor:in) / Jenny, R. W. (Autor:in)

    Erscheinungsdatum :

    24.06.1974


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :