Problems of detecting fire and overhead in supersonic aircraft, while similar to those in subsonic aircraft, have certain unique characteristics; characteristics are due basically to dynamic and thermal environment associated with Mach 3 to Mach 4.5 flight regime; approach toward solution of these problems and history of aircraft fire and overheat detection leading to current system design concepts are presented.


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    Title :

    Fire detection techniques for supersonic aircraft


    Additional title:

    ASME -- Paper


    Contributors:
    Beery, G.T. (author) / Trumble, T.M. (author)

    Conference:

    ASME Meeting GT42 ; 1968 Supersonic



    Publication date :

    1968


    Size :

    5 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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