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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 ...
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 first prototype, the V1 (D-AANA), was fitted with 680hp Junkers Jumo 210Da engines. The second prototype, V-2, was fitted with 670hp Jumo 210G engines [1] R. Blaser was assigned to detail design. In order to improve performance compared with the Bf 110, the fuselage was made as small as possible.
The Jumo 210D was replaced with the new fuel-injected 210Ga, which improved performance of the engine to 522 kW (700 hp) for takeoff, and a sustained output of 503 kW (675 hp) at the reasonably high altitude of 4,700 m (15,420 ft). Better yet, the Ga also decreased fuel consumption, thus increasing the aircraft's endurance.
Variants included the D-0 and D-1 models, both having a Junkers Jumo 210D engine and armed with two wing-mounted and two nose-mounted 7.92 mm (.312 in) MG 17s. The D-2 was an experimental version with an engine-mounted machine gun, but as previously tried, this installation failed.
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 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 ...