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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.
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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 ...
It was originally designated Ta 211 in reference to the intended Jumo 211R engine, although it was subsequently decided to adopt the more powerful Jumo 213 powerplant instead. Following a review of Focke-Wulf's submission, a development contract was issued to the company during late 1942.
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The Ju 188 was designed to be fitted with either the 1,750 PS (1,290 kW; 1,730 hp) Jumo 213A or 1,700 PS (1,250 kW; 1,680 hp) BMW 801 G-2 engines without any changes to the airframe, with the exclusion of the re-design for Jumo-powered examples, of the annular radiators from their Jumo 211 layout for the A-series to better match the more ...
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 ...