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The Junkers J.I (manufacturer's name J 4) was a German "J-class" armored sesquiplane of World War I, developed for low-level ground attack, observation and army cooperation. It is especially noteworthy as being the first all-metal aircraft to enter mass production; the aircraft's metal construction and heavy armour was a shield against small ...
Junkers EF 082, combat battle aircraft project. Junkers EF 094, design designation for Ju 322. Junkers EF 100, six-engine, wide-body transatlantic airliner, 1940; Junkers EF 101, Mistel aircraft design; Junkers EF 112, twin-boom ground attack aircraft project, 1942. Junkers EF 115, bomber project with four Jumo 211 engines or 2 jet engines
Junkers J 5. The Junkers J 5 was a ... In early 1917, Junkers developed at least two cantilever wing monoplane fighter aircraft designs based on the J4. [1] J 5I. The ...
Pages in category "Junkers aircraft" The following 59 pages are in this category, out of 59 total. This list may not reflect recent changes. A. Junkers A 32;
The aircraft was known only by its Junkers factory model number of J 1 and should not be confused with the later, armoured all-metal Junkers J 4 sesquiplane, accepted by the later Luftstreitkräfte as the Junkers J.I (using a Roman numeral), from the category of armored combat aircraft established by IdFlieg.
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 ...
Pages in category "Junkers aircraft engines" The following 16 pages are in this category, out of 16 total. This list may not reflect recent changes. 0–9.
The Junkers J 2's pioneering "unitized" forward fuselage structure, integrating the wing roots, engine mount and cockpit. The J 2 differed from the J 1 in having a cowling that almost entirely enclosed the engine, a rounded upper and lower fuselage section instead of the rectangular section of the J 1., and a narrower and deeper ventral radiator enclosure, and had a horizontal stabilizer ...