Description
Jumo 211 exhausts The Jumo 211 was a supercharged liquid-cooled 60-degree inverted V 12 piston aircraft engine, Junkers Motoren's primary aircraft engine of World War II. It was primarily used in HYPERLINK ' https://en.wikipedia.org/wiki/Bomber ' o 'Bomber' bombers such as Junkers HYPERLINK ' https://en.wikipedia.org/wiki/Junkers_Ju_87 ' o 'Junkers Ju-87' Ju-87 and HYPERLINK ' https://en.wikipedia.org/wiki/Junkers_Ju_88 ' o 'Junkers Ju-88' Ju 88, and HYPERLINK ' https://en.wikipedia.org/wiki/Heinkel_He_111 ' o 'Heinkel He 111' Heinke l He 111 medium bomber. It was the most-produced German aero engine of the war, with almost 70,000 examples completed. It displaced 2,135 cu in. It developed 986 hp at 2,200 rpm on take-off (Jumo 211C). Applications: Avia S-199/CS-199 Dornier Do-217 - single engine test aircraft Focke-Wulf Ta-154 Heinkel He-111E, He-111H and He-111Z I.A.R. 79 Junkers F 24kai Jumo 211 test bed Junkers Ju-87 'Stuka' Junkers Ju-88 Junkers Ju-90 Junkers Ju-252 Messerschmitt Me-264 (V1 prototype only) Messerschmitt Me-323 (only for tests) Savoia-Marchetti SM.79 (Romanian variants) (designed to be used with kits made by many kit manufacturers including Airfix, Academy, Fujimi, Heller, Italeri, Revell kits)