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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.
The Jumo 211 became the major bomber engine of the war, in no small part due to Junkers also building a majority of the bombers then in use. Of course, since it was the Luftwaffe that selected the final engine to be used after competitive testing on prototypes (such as the Dornier Do 217), there is certainly more to it. Limited production ...
The V20 used the same Jumo 213E engine as the Fw 190D-9, while the V21 used the DB 603E. Neither of these offered any significant improvement over the Fw 190D-9, and further development of the Ta 152A and B was cancelled. The V21 airframe was further modified as the V21/U1 and became the prototype for the Ta 152C. [2]
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The fighter chosen was the Focke-Wulf Ta 152H, a derivative of the Fw 190D with a longer wingspan and powered by the new high-altitude model "E" of the Junkers Jumo 213 engine. An alternative fighter model was the Messerschmitt Me 155B , a long- winged development of the Bf 109 , which had already undergone several stages of design and would ...
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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. In this design, the compressor, combustion chamber and turbine are traversed in axial direction by the air taken directly from the inlet.