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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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Junkers Jumo 205C-4 (660 hp) Junkers Jumo 210C (600 hp) Junkers Jumo 210Ca (640 hp) Junkers Jumo 210G (700 hp) Junkers Jumo 210Ea (680 hp) Junkers L5 (280 hp) Klimov M-103 (960 hp) Klimov M-105PF (1,210 hp) Lorraine-Dietrich 12Eb (450 hp) Lorraine 12Hfrs Petrel (780 hp) Lorraine 12Hgrs Petrel (780 hp) Menasco L-365-1 (125 hp) Pratt & Whitney R ...
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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Jumo 213 improved Jumo 211, inverted V-12; Jumo 222 key engine program for German military aircraft: experimental 24-cylinder supercharged liquid-cooled "star" (6 banks, of 4 cylinders apiece) aircraft engine; nearly 300 examples built; Jumo 223 "box" engine made of four 207s; Jumo 224 "box" engine made of four 208s. Siemens–Schuckert Werke
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