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A Junkers W33 was flown with a 680 hp version of the Jumo 210 on 5 July 1934. [2] Initial production of the 610 PS (602 hp, 449 kW) Jumo 210A started in late 1934. Further development led in 1935 to the 640 PS (631 hp, 471 kW) 210B and 210C. Both added a new supercharger for improved performance, along with a dump valve to avoid overboost. The ...
While the Daimler-Benz engine was mostly used in single-engined and twin-engined fighters, the Jumo engine was primarily used in bombers such as Junkers' own Ju 87 and Ju 88, and Heinkel's H-series examples of the Heinkel He 111 medium bomber. It was the most-produced German aero engine of the war, with almost 70,000 examples completed.
The Junkers Ju 87, popularly known as the "Stuka", [b] is a German dive bomber and ground-attack aircraft.Designed by Hermann Pohlmann, it first flew in 1935.The Ju 87 made its combat debut in 1937 with the Luftwaffe's Condor Legion during the Spanish Civil War of 1936–1939 and served the Axis in World War II from beginning to end (1939–1945).
The Jumo 205 aircraft engine was the most numerous of a series of aircraft diesel engines produced by Junkers.The Jumo 204 first entered service in 1932. Later engines of this type comprised the experimental Jumo 206 and Jumo 208, with the Jumo 207 produced in some quantity for the Junkers Ju 86P and -R high-altitude reconnaissance aircraft, and the 46-meter wingspan, six-engined Blohm & Voss ...
G-6 versions were equipped with 1,287 kW (1,726 hp) Jumo 213A inverted V-12 engines (using the same redesigned annular radiator cores as the Ju 188s powered by them), enlarged fuel tanks and often one or two 20 mm (0.79 in) MG 151/20 cannons in a Schräge Musik ("Jazz Music", i.e. slanted) installation. These guns were pointed obliquely upwards ...
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 ...
Fuel capacity: 1,500 L (400 US gal; 330 imp gal) in two fuselage tanks; Powerplant: 2 × Junkers Jumo 213E V-12 inverted liquid-cooled piston engines, 1,305 kW (1,750 hp) each for take-off; 984 kW (1,320 hp) at 10,000 m (33,000 ft) Propellers: 3-bladed Junkers VS-9 wooden constant-speed propellers; Performance
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.