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 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 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 …

Power rating: 1,268 kW (1,700 hp) at 2,700 rpm. Displacement: 36.9 L (2,250 cu in.) Bore and Stroke: 154 mm (6.06 in.) x 165 mm (6.50 in.) Weight: 701 kg (1,543 lb) In 1933, Junkers …

Junkers Jumo 213A-1, Inverted V-12 Engine In 1933, Junkers began the development of a series of high-power gasoline-powered engines. The first of these were the Jumo 210 and 211, liquid …

May 11, 2008 · The Jumo 213 was being developed specifically with the very complex supercharging system characteristic of the 213E from the very beginning and the 213A was a …

Der Jumo 213 ist die direkte Weiterentwicklung vom Jumo 211 und hat die gleichen Zylinderabmessung wie der Jumo 211, aber gegenüber dem Jumo 211 wurde das Triebwerk …

Nov 11, 2013 · New developments and major changes used in the Jumo-213 engine were: Water cooled cylinder heads; adjustment of the gas distribution mechanism; on each cylinder 1 …

The Jumo 213 is a further development of the Jumo 211 and was designed by Dr. Lichte. It was smaller than the Jumo 211, performed a higher turn rate and offered more power. It had a …

Der Junkers Jumo 213 war ein flüssigkeitsgekühlter Zwölfzylinder-Flugmotor mit Benzindirekteinspritzung und 35 Litern Hubraum der Junkers Flugzeug- und Motorenwerke. Er …