A flight propulsion system preliminary design was established that meets the program goals of at least a 12 percent reduction in thrust specific fuel consumption, at least a five percent reduction in direct operating cost, and one-half the performance deterioration rate of the most efficient current commercial engines. The engine provides a high probability of meeting the 1978 noise rule goal. Smoke and gaseous emissions defined by the EPA proposed standards for engines newly certified after 1 January 1981 are met with the exception of NOx, despite incorporation of all known NOx reduction technology.


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    Titel :

    Energy Efficient Engine Flight Propulsion System Preliminary Analysis and Design Report


    Beteiligte:
    W. B. Gardner (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    480 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch