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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 ...
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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.
The -2 would use the 46.4 litre displacement, 1,864 kW (2,500 hp) Jumo 222A/B 24-cylinder six-bank liquid-cooled engines, or the identical displacement 222E/F versions with an improved two-speed supercharger with triple intercoolers on each engine. The -3 would mount the Junkers Jumo 213E liquid-cooled inverted V12, which included a ...
5 D-1 with Jumo 213E (prototypes), engine installation tested in A-2 fuselelage; Source is stated as Ernst Heinkel AG delivery plan from December 15, 1944 with deliveries as of December 11, 1944. --Denniss 22:48, 28 July 2006 (UTC) I believe those numbers are orders, not actual production.