The potential of using liquid hydrogen as fuel in subsonic transport aircraft was investigated to explore an expanded matrix of passenger aircraft sizes. Aircraft capable of carrying 130 passengers 2,780 km (1500 n.mi.); 200 passengers 5,560 km (3000 n.mi.); and 400 passengers on a 9,265 km (5000 n.mi.) radius mission, were designed parametrically. Both liquid hydrogen and conventionally fueled versions were generated for each payload/range in order that comparisons could be made. Aircraft in each mission category were compared on the basis of weight, size, cost, energy utilization, and noise. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Study of LH2 Fueled Subsonic Passenger Transport Aircraft


    Beteiligte:
    G. D. Brewer (Autor:in) / R. E. Morris (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    186 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Study of LH2 fueled subsonic passenger transport aircraft

    Brewer, G. D. / Morris, R. E. | NTRS | 1976



    Study of fuel systems for LH2-fueled subsonic transport aircraft, volume 2

    Brewer, G. D. / Morris, R. E. / Davis, G. W. et al. | NTRS | 1978


    Study of Fuel Systems for LH2-Fueled Subsonic Transport Aircraft, Volume 2

    G. D. Brewer / R. E. Morris / G. W. Davis et al. | NTIS | 1978


    Advanced subsonic aircraft concepts for passenger transportation

    Waters, M. H. / Williams, L. J. | NTRS | 1975