Comet 4 will have all-up weight of 152,500 lb and has four Avon engines of 10,500 lb thrust; capacity payload of first class version is 16,500 lb (60 passengers), and that of tourist version, 19,300 lb (76 passengers); structural design test program; factors in favor of wing engine installation; control system. (see also Flight v 69 n 2469 May 18 1956 p 607-9)


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    Titel :

    Comet 4 -- Design and operational considerations


    Weitere Titelangaben:

    Can Aeronautical J


    Beteiligte:
    Bishop, R.E. (Autor:in) / Cunningham, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1956


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Comet 4 -- Design and operational considerations

    Bishop, R.E. / Cunningham, J. | Engineering Index Backfile | 1956



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