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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.
Data from Jane's Fighting Aircraft of World War II [1]. General characteristics. Crew: two Wing area: 42 m 2 (450 sq ft) Gross weight: 11,490 kg (25,331 lb) Powerplant: 2 × Junkers Jumo 213E inverted V-12 liquid-cooled piston engines, 1,300 kW (1,750 hp) each with a three-speed two-stage intercooled supercharger, 2,050 hp (1,530 kW) with MW 50 boost
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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 ...
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On 1 July 1943, the prototype Ta 154 V1, which was outfitted with Jumo 211F engines and bore the Stammkennzeichen identification code TE+FE, performed its maiden flight in the hands of Kurt Tank. [5] It was followed by V2 with Jumo 211N engines, which was kept at the factory for handling trials.