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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
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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The larger wings allowed the gear to retract directly to the rear. A new universal engine mount would allow for the use of any of the DB 603JZ or BMW 801J turbocharged engines or the Jumo 213E two-stage mechanically supercharged engines, driving a new four-blade propeller with very wide blades.
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 ...