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Initially, Junkers proposed modifications of the Jumo 004, specifically the 109-004G and 109-004H. However, these variants were rejected as they were not powerful enough, and Junkers began to design the 109-012. [1] The engine was to feature an 11-stage axial compressor enclosed in a sheet-steel casing and a 2-stage, air-cooled turbine.
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
The Jumo 211 was a German inverted V-12 aircraft engine, Junkers Motoren's primary aircraft engine of World War II.It was the direct competitor to the Daimler-Benz DB 601 and closely paralleled its development.
Pages in category "Junkers aircraft engines" ... This list may not reflect recent changes. 0–9. Junkers Jumo 012; J. Junkers Jumo 004; Junkers Jumo 204; Junkers ...
The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211.The design added two features, a pressurized cooling system that required considerably less cooling fluid which allowed the engine to be built smaller and lighter, and a number of improvements that allowed it to run at higher RPM.
Citations: Mewes 1997, p. 36-39. It was designed as a single-shaft, single-flow turbojet. The basic conception was a further development of the design already applied with high perfection on Junkers Jumo 004 and Junkers Jumo 012, as well as the BMW 003 and BMW 018 engines.
The Junkers Jumo 012 engine is tested, it stands as the most powerful engine in the world for some time, at 6,600 lbf (29,000 N). The J35, a development of an earlier turboprop effort, runs for the first time. Ford builds a copy of the V-1's engine, known as the PJ-31-1. The Ishikawajima Ne-20 first runs in Japan. Originally intending to build ...
The Jumo 210G was rated at 730 PS (720 hp, 534 kW) and was only available for fast aircraft like the Bf 109 and Bf 110 but not for slow aircraft like the Ju 87. Further developments were planned as Jumo 210F and 210H, but never built. In 1935 the Jumo 210H, with twin exhaust valves for each cylinder, was used for development of the Jumo 211.