Several devices are equally satisfactory in reversing or modulating thrust; therefore, other considerations, such as inherent fail safe characteristics, ease of installation, weight and performance penalty to aircraft, actuation power requirements, compatibility with silencer nozzles and other components of exhaust system, must serve as basis for selection; functional practicability of thrust reverser installation demonstrated on Allison J-71 engine.


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    Title :

    Thrust-reverser devices


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1957


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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