Design and performance data of experimental low-wing monoplane built by Gloucester Aircraft Co.; structure weight is only 26 per cent of total weight; two 40-hp. Salmson 9-cylinder radial engines; full loaded machine weighs 1800 lb. of which 1057 lb. is tare weight; top speed 110 m.p.h.; span 38 ft. (see also Aeroplane, vol. 41, no. 2, July 8, 1931, pp. 122-126, 8 figs; Nat. Advisory Committee Aeronautics -- Aircraft Cir., no. 148, July 1931, 7 pp., 8 figs. on supp. plates)
First mono-spar monoplane
Flight
Flight ; 23 , n 28
1931
4 pages
7 Figs.
Article (Journal)
English
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Engineering Index Backfile | 1931
Engineering Index Backfile | 1931
Engineering Index Backfile | 1929
Engineering Index Backfile | 1932