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  2. Junkers Jumo 210 - Wikipedia

    en.wikipedia.org/wiki/Junkers_Jumo_210

    In 1936 the new 670 PS (661 hp, 493 kW) 210D and 210E were introduced, which had the same gearing as the B and C but used a new two-speed supercharger to increase takeoff power and altitude performance. The Jumo 210G had a direct injection system developed by August Lichte. The Jumo system used a small pump piston positioned beside each of the ...

  3. Junkers Jumo 211 - Wikipedia

    en.wikipedia.org/wiki/Junkers_Jumo_211

    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.

  4. Category:Junkers aircraft engines - Wikipedia

    en.wikipedia.org/wiki/Category:Junkers_aircraft...

    Junkers Jumo 222; Junkers Jumo 223; L. Junkers L1; Junkers L2; Junkers L5; Junkers L8; Junkers L55; Junkers L88; P. Pirna 014 This page was last edited on 30 May 2024 ...

  5. Junkers Jumo 205 - Wikipedia

    en.wikipedia.org/wiki/Junkers_Jumo_205

    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 ...

  6. BMW 003 - Wikipedia

    en.wikipedia.org/wiki/BMW_003

    The few Messerschmitt Me 262 A-1b test examples built used the more developed version of the 003 jet, recording an official top speed of 500 mph (800 km/h). The Me 262A-1a production version used the competing Jumo 004, whose heavier weight required the wings to be swept back in order to move the center of gravity into the correct position.

  7. Junkers Jumo 213 - Wikipedia

    en.wikipedia.org/wiki/Junkers_Jumo_213

    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.

  8. Junkers Jumo 204 - Wikipedia

    en.wikipedia.org/wiki/Junkers_Jumo_204

    The Jumo 204 was an opposed-piston, inline, liquid-cooled 6-cylinder aircraft Diesel engine produced by the German manufacturer Junkers. It entered service in 1932. It entered service in 1932. Later engines in the series, the Jumo 205 , Jumo 206 , Jumo 207 and Jumo 208 , differed in stroke, bore, and supercharging arrangements.

  9. Junkers Jumo - Wikipedia

    en.wikipedia.org/?title=Junkers_Jumo&redirect=no

    Junkers#Junkers Jumo To a section : This is a redirect from a topic that does not have its own page to a section of a page on the subject. For redirects to embedded anchors on a page, use {{ R to anchor }} instead .