Detailed illustrated description of World's fastest aircraft in production; oa length 41 ft 2 in.; wing span 54 ft 2 in.; wing area 436 sq ft; normal loaded weight, 18,540 lb; power plant consists of two Rolls-Royce Merlin XXI engines, each developing 1260 bhp. June: Details of molded, split fuselage construction and wing spar manufacture. July: Wing assembly; tailplane, fin and flaps; undercarriage; final assembly. (See also - n 56 June p 262-73)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    De Havilland Mosquito


    Additional title:

    Aircraft Production


    Contributors:
    Goff, W.E. (author)

    Published in:

    Publication date :

    1943


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    De Havilland mosquito

    Bourdon, M.W. | Engineering Index Backfile | 1943


    De Havilland mosquito XVI

    Engineering Index Backfile | 1945


    Story of De Havilland "Mosquito"

    Engineering Index Backfile | 1944


    De Havilland "mosquito" bomber and fighter

    Engineering Index Backfile | 1943


    De Havilland "mosquito" bomber and fighter

    Engineering Index Backfile | 1943