This study was conducted to ascertain potential benefits of a propfan propulsion system application to a blended wing/body military tactical transport. Based on a design cruise Mach no. of 0.75 for the design mission, the results indicate a significant advantage in various figures of merit for the propfan over those of a comparable technology turbofan. Although the propfan has a 1.6 percent greater takeoff gross weight, its life cycle cost is 5.3 percent smaller, partly because of a 27 percent smaller specific fuel consumption. When employed on alternate missions, the propfan configuration offers significantly improved flexibility and capability: an increase in sea level penetration distance of more than 100 percent, or in time-on-station of 24 percent, or in deployment payload of 38 percent.


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    Titel :

    Multiple Application Propfan Study (MAPS): Advanced tactical transport


    Beteiligte:
    Newton, F. C. (Autor:in) / Liebeck, R. H. (Autor:in) / Mitchell, G. H. (Autor:in) / Mooiweer, A. (Autor:in) / Platte, M. M. (Autor:in) / Toogood, T. L. (Autor:in) / Wright, R. A. (Autor:in)

    Erscheinungsdatum :

    1986-03-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    F. C. Newton / R. H. Liebeck / G. H. Mitchell et al. | NTIS | 1986


    Multiple-Purpose Subsonic Naval Aircraft (MPSNA): Multiple Application Propfan Study (MAPS)

    Engelbeck, R. M. / Havey, C. T. / Klamka, A. et al. | NTRS | 1986


    Multiple-Purpose Subsonic Naval Aircraft (Mpsna): Multiple Application Propfan Study (Maps)

    R. M. Engelbeck / C. T. Havey / A. Klamka et al. | NTIS | 1986