Tandem-cockpit, parasol-type plane for sport and instruction purposes has been developed by Doyle Aero Corp., Baltimore, Md.; wing span 30 ft.; top speed 130 m.p.h.; landing speed 41 m.p.h.; fuselage structure is of seamless steel tubing at all joints to form single unit; cabane structure is welded direct to fuselage and designed to take loads; wing of wood and duralumin. (see also Airway Age, vol. 10, no. 4, Apr. 1929, pp. 514 and 516, 2 figs.; Aviation Eng., vol. 2, no. 4, Apr. 1929, pp. 32-33, 2 figs.; Aero Digest, vol. 14, no. 4, Apr. 1929, p. 126, 2 figs.; and Aero Digest, vol. 14, no. 2, Feb. 1929, p. 122, 1 fig.)
The "Oriole" monoplane
Aviation
Aviation ; 26 , n 12
1929
2 pages
5 Figs.
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
Fragmentation Test of Warhead No. 145 for Oriole Missile
NTIS | 1953
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