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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.
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 Junkers Ju 187 was a German projected dive bomber designed to replace the ageing ... × 1 Junkers Jumo 213A V-12 inverted liquid-cooled piston engine ...
The Ju 188 was designed to be fitted with either the 1,750 PS (1,290 kW; 1,730 hp) Jumo 213A or 1,700 PS (1,250 kW; 1,680 hp) BMW 801 G-2 engines without any changes to the airframe, with the exclusion of the re-design for Jumo-powered examples, of the annular radiators from their Jumo 211 layout for the A-series to better match the more ...
Junkers Jumo 213A inverted V12 engines with 1,287 kW (1,726 hp), used either FuG 220 Lichtenstein SN-2 90 MHz or FuG 218 Neptun 158/187 MHz frequency radar, either with the usual Hirschgeweih eight-dipole aerial setup or experimentally with the more aerodynamic Morgernstern tripled crossed-dipole aerials.
Unfortunately for the design team, the Me 209's proposed DB 603A engine was in short supply and they were forced to use the Junkers Motorenwerke firm's Jumo 213A engine. Even though the 35-litre engine displacement Jumo 213 had been deliberately designed to have as many of its engine access points as possible made to be identical with the 44.52 ...
Speaking to the technical director in charge of the inverted V12, liquid-cooled Junkers Jumo 213's development, the Mission learned there were many experimental variants, but only three [definitive] models: the 213A (the major production version), the 213E (a high-altitude model), and the projected 213J (improved still more). [35]