Airforce

Wright Cyclone R 2600 Aircraft Engine,Specifications (USA)

Wright Cyclone R 2600 Aircraft Engine Technical Details Working volume-29.8 liters Compression ratio-6.4 Weight-595 kg Diameter-1400 mm Cylinder diameter-174.6 mm Take-off power – 1400 hp Wright Cyclone R 2600 Aircraft Engine In 1909, the world-famous pioneers of aviation, the American brothers Wilbur and Orville Wright, founded the company for the production of aircraft engines. Initially, …

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Allison V-1710 Aircraft Engine,Technical Specifications (USA)

Allison V-1710 Aircraft Engine Technical Specifications Working volume-28 l Compression ratio-6.5 Weight-650 kg Length-744 mm Height-928 mm Cylinder diameter-139.7 mm Take-off power – 1165 hp Allison V-1710 Aircraft Engine Details The first aircraft engine for the US Army Air Force was developed by Allison in 1924. It was an experimental 24-cylinder air-cooled engine with an …

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Kawasaki Ki-48 Bomber Aircraft, Technical Specifications – Japan

Kawasaki Ki-48 Bomber Aircraft Technical Specifications Crew – 4 people Engine – ” Nakajima Na. 115 Power – 1150 hp Wingspan-17.45 m Wing area – 40.0 sq. m Empty aircraft weight-4550 kg Maximum take-off weight-6,750 kg Maximum speed at altitude/near the ground – 505/350 km / h Practical ceiling – 10,100 m Maximum range-2400 km …

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Cabin of a Junkers Ju 88a1 Bomber Aircraft, Germany

Cabin of a Junkers Ju 88a1 Bomber Aircraft Technical Specifications Crew – 4 people Engine-Jumo 211 In-1 Power-1200 hp Wingspan-18.4 m The wing area is 52.5 sq. m Empty aircraft weight-7700 kg Maximum take-off weight-10,400 kg Maximum speed at altitude/near the ground-450 / 350 km / h Practical ceiling – 9800 m Maximum range-1690 km …

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