Data are tabulated for two conceptual engines designed for small transport aircraft. These are the 1790 W (2400 shp) class engine and the 3579 kW (4800 shp) class engine for the 0.5 M sub N and 0.7 M sub N airplanes, respectively. All data points required to perform the STAT missions are provided including take-off, climb, cruise, loiter, and fuel allowances. The weight, dimensions, price, and maintenance costs are given as well as the installation criteria and equations used for adjusting horsepower for gearbox loss, and converting horsepower to thrust. Scaling equations are included.


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    Title :

    Propulsion Study for Small Transport Aircraft Technology (STAT), Appendix B


    Publication date :

    1980


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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