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Stipa-Caproni tubular monoplane with cylindrical fuselage; wings are attached to sides of tube or cylinder; pilot and passenger seats are on top, engine is inside of tube, and propeller is located at front end; weight empty, 600 kg; wing span 14.3 m, length 5.9 m. See also Engineering Index 1932 p 22 and 23. (German translation) (See also Politecnico v 81 n 2 Feb 1933 p 106-9; French translation in Genie Civil v 103 n 4 July 22 1933 p 91 and English translation in Mech Eng v 55 n 10 Oct 1933 p 631-2)
Stipa-Caproni tubular monoplane with cylindrical fuselage; wings are attached to sides of tube or cylinder; pilot and passenger seats are on top, engine is inside of tube, and propeller is located at front end; weight empty, 600 kg; wing span 14.3 m, length 5.9 m. See also Engineering Index 1932 p 22 and 23. (German translation) (See also Politecnico v 81 n 2 Feb 1933 p 106-9; French translation in Genie Civil v 103 n 4 July 22 1933 p 91 and English translation in Mech Eng v 55 n 10 Oct 1933 p 631-2)
Stipa-Caproni tubular monoplane
L'aereo-tubolare Stipa
Silvestri, A. (author)
1933
2 pages
Article (Journal)
German
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Engineering Index Backfile | 1921
Engineering Index Backfile | 1921
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Engineering Index Backfile | 1927
| Engineering Index Backfile | 1927