Search results
Results From The WOW.Com Content Network
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.
Powerplant: 1 × Junkers Jumo 213E or Junkers Jumo 213E-1 V-12 inverted liquid-cooled piston engine, 1,287 kW (1,726 hp) for take-off; 1,530 kW (2,050 hp) for take-off with MW-50 water/methanol injection 940 kW (1,260 hp) at 10,700 m (35,100 ft) with GM-1 Nitrous Oxide injection. Propellers: 3-bladed Junkers VS-9 constant-speed propeller ...
Main bomber type with Jumo 211 engines. Ju 88 A-0 Pre-production aircraft. Ju 88 A-1 Initial production variant. 895 kW (1,200 hp) Jumo 211B-1 engines Ju 88 A-2 Jumo 211 G-1 engines. Ju 88 A-3 Conversion trainer. Dual controls and throttles, various instruments duplicated. The rear-facing defensive armament of the Ju 88 A-4. Ju 88 A-4 Improved ...
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. Limited production ...
Pages for logged out editors learn more. Contributions; Talk; Junkers Jumo 213E
Main page; Contents; Current events; Random article; About Wikipedia; Contact us; Pages for logged out editors learn more
On 1 July 1943, the prototype Ta 154 V1, which was outfitted with Jumo 211F engines and bore the Stammkennzeichen identification code TE+FE, performed its maiden flight in the hands of Kurt Tank. [5] It was followed by V2 with Jumo 211N engines, which was kept at the factory for handling trials.
Data from Die Deutsche Luftrüstung 1933–1945 Vol.3 – Flugzeugtypen Henschel-Messerschmitt General characteristics Crew: 3 Length: 15.2 m (49 ft 10 in) Wingspan: 22 m (72 ft 2 in) Height: 4.35 m (14 ft 3 in) Wing area: 56 m 2 (600 sq ft) Max takeoff weight: 14,000 kg (30,865 lb) Powerplant: 2 × BMW 801J 14-cylinder air-cooled radial piston engine, 1,350 kW (1,810 hp) each Propellers: 4 ...