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There was a significant size difference between the upper and lower wings – the upper wing had an area of 35.89 m 2 (386.3 sq ft), over double the area of the lower wing – 13.68 m 2 (147.3 sq ft). [5] This is a form of biplane known as a sesquiplane. The aircraft had two fuel tanks with a capacity of around 120 litres (32 US gal). [5]
Junkers T 26, training and sports aircraft, 1925. Junkers T 27, a re-engined T 26, 1925. Junkers J 28, two-seat version of T.21, not built. Junkers J 29, sports monoplane, double wing development aircraft, 1925. Junkers K 30, military version of G 24, 1930. Junkers G 31, 15 seat airliner, 1926. Junkers A 32, experimental monoplane, 1926.
The Junkers Ju 87, popularly known as the "Stuka", [b] is a German dive bomber and ground-attack aircraft.Designed by Hermann Pohlmann, it first flew in 1935.The Ju 87 made its combat debut in 1937 with the Luftwaffe's Condor Legion during the Spanish Civil War of 1936–1939 and served the Axis in World War II from beginning to end (1939–1945).
The Junkers G.38 was a large German four-engine transport aircraft that first flew in 1929. [1] Two examples were constructed in Germany. Both aircraft flew as a commercial transport within Europe in the years leading up to World War II .
Print/export Download as PDF; Printable version; In other projects ... Pages in category "Junkers aircraft" The following 59 pages are in this category, out of 59 ...
The Junkers Ju 390 was a German long-range derivative of the Junkers Ju 290 aircraft, intended to be used as a heavy transport aircraft, maritime patrol aircraft and long-range bomber. It was one of the aircraft designs submitted for the abortive Amerikabomber project, along with the Messerschmitt Me 264 , the Focke-Wulf Ta 400 and the Heinkel ...
Print/export Download as PDF; Printable version; ... Pages in category "Junkers aircraft engines" The following 16 pages are in this category, out of 16 total.
Nearly 5,000 Junkers Ju 52/3m were built, the most of any trimotor. A trimotor is a propeller-driven aircraft powered by three internal combustion engines, characteristically one on the nose and one on each wing. A compromise between complexity and safety, such a configuration was typically a result of the limited power of the engines available ...