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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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Created Date: 8/30/2012 4:52:52 PM
The V20 used the same Jumo 213E engine as the Fw 190D-9, while the V21 used the DB 603E. Neither of these offered any significant improvement over the Fw 190D-9, and further development of the Ta 152A and B was cancelled. The V21 airframe was further modified as the V21/U1 and became the prototype for the Ta 152C. [2]
Download as PDF; Printable version; ... Junkers Jumo 004; Junkers Jumo 204; ... Category: Junkers aircraft engines. 5 languages ...
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 Junkers Jumo 223 was an experimental 24-cylinder aircraft engine based on the Junkers Jumo 205.Like the Jumo 205, it was an opposed piston two-stroke diesel engine. It had four banks of six cylinders in a rhomboid configuration, with four crankshafts, one at each vertex of the rhombus, and 48 pistons.