In this study, new technology engines were defined in two power classes: a 200 hp class, for a light, 4-place personal aircraft, and a 1500 pound thrust class for a twin-engined, 6 place business jet type aircraft. The engines were evaluated for retrofitting suitable current production aircraft for comparison to the existing engines. The engines were evaluated for performance using a typical mission for each aircraft, as well as a variant mission to further appraise performance.Issues of cost, safety, maintenance, and reliability were also addressed. Manufacturing plans were then constructed.


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    Titel :

    Advanced Propulsion System Studies for General Aviation Aircraft


    Beteiligte:

    Erscheinungsdatum :

    2003-08-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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