Some important base line requirements for commercial aircraft propulsion systems; in summary, engines must be designed to be installed in aircraft not on test stand; decision must be directed toward long life, ease of repair, and good long term installed performance; all power plant subsystems must be integrated into installation, tested early and throughly as part of power plant, and be more reliable and maintainable than current equipment in service. (15346)


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    Title :

    Design requirements and objectives for commercial aircraft propulsion systems


    Additional title:

    ASME Paper


    Contributors:

    Conference:

    ASME Meeting GT-57 ; 1969 Design



    Publication date :

    1969


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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