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The Junkers Jumo 004 was the world's first production turbojet engine in operational use, and the first successful axial compressor turbojet engine. Some 8,000 units were manufactured by Junkers in Germany late in World War II, powering the Messerschmitt Me 262 fighter and the Arado Ar 234 reconnaissance/bomber, along with prototypes, including the Horten Ho 229.
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.
The 003 and the Junkers Jumo 004 were the only German turbojet engines to reach production during World War II. Work had begun on the design of the BMW 003 before its contemporary, the Jumo 004, but prolonged developmental problems meant that the BMW 003 entered production much later, and the aircraft projects that had been designed with it in ...
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 Junkers Jumo 109-012, known colloquially post-war as Jumo 012, was a turbojet engine under development in Germany during the Second World War.In essence, it was a scaled up version of the Jumo 004 (the Jumo 004 had already reached serial production by 1944).
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.
Pages in category "Junkers aircraft engines" The following 16 pages are in this category, out of 16 total. ... Junkers Jumo 204; Junkers Jumo 205; Junkers Jumo 210;
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.