Twin-engined biplane bomber; aerodynamic design; structural design; system of standardizing certain spar flanges, webs and fittings in sufficient number of combinations; simple 2-wheeled undercarriage; diagram of oleo-pneumatic telescopic "legs" of unusual design. July 5: All-metal three-seater high-performance bomber powered with two Bristol Jupiter VI engines, mounted on lower wings, giving total of 900 hp.; machine guns in forward gun turret in nose; wing span 75 ft.; maximum speed 130 m.p.h.; fuselage of locked-joint type tubes made from flat steel strips. (See also Flight vol. 20, nos. 13 and 27, Mar. 29 pp. 206-213 and 541 24 figs; Aeroplane, vol. 34, no. 13, Mar. 28, 1928, pp. 418, 420, 421, and 422; also Aviation, vol. 25, no. 1, July 2, 1928, p. 33, 1 fig)


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    Title :

    Boulton and paul, The boulton and paul "sidestrand I."


    Additional title:

    Airways


    Published in:

    Airways ; 4 , n 7


    Publication date :

    1928


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





    Boulton and Paul. Boulton and Paul, Ltd

    Engineering Index Backfile | 1929