Back Junkers Jumo 213 Czech Junkers Jumo 213 German Junkers Jumo 213 Spanish یونکرس یومو ۲۱۳ Persian Junkers Jumo 213 French Junkers Jumo 213 Hungarian Junkers Jumo 213 Italian ユンカース ユモ 213 Japanese Junkers Jumo 213 Portuguese Junkers Jumo 213 Swedish
| Jumo 213 | |
|---|---|
| |
| Junkers Jumo 213 | |
| Type | Piston inverted V-12 aero-engine |
| Manufacturer | Junkers |
| First run | 1940 |
| Major applications | Focke-Wulf Fw 190D Focke-Wulf Ta 152 Junkers Ju 188 |
| Number built | 9,000 |
| Developed from | 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 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. These changes boosted power by over 500 hp and made the 213 one of the most sought-after Axis engine designs in the late-war era.