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. (see also German translation in Schweiz Bauzeitung v 102 n 1 July 1933 p 8-9; 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
Politecnico ; 81 , n 2
1933
4 pages
Aufsatz (Zeitschrift)
Italienisch
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Stipa-Caproni tubular monoplane
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