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Technical Specifications Junkers Ju-52 |
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Manufacturer: Year: Passenger seats: Volume of fuel tank: Fuel consumption: Max. flight time:
Engine: BMW 132A/3 Take-off power: Max. engine speed: Propeller pitch fixed:
Dimensions and weights: Span width: Over-all length: Over-all height: Basic weight: Max. take-off weight: Max. payload:
Speed: Take-off speed: Cruising speed: Landing speed: Max. altitude: Take-off distance: Landing distance: |
Junkers, Germany 1939 17 2500 Liter (= 660 gallon US) 380 Liter/h (= 100 gallon US/h) 6 h
9 cylinders, 4-stroke radial engine 650 PS 2050 rpm 19°
29.25 m (= 96 ft) 18.90 m (= 62 ft) 6.10 m (= 20 ft) 7000 kg (= 7.7 tons US) 10500 kg (= 11.5 tons US) 3500 kg (= 3.9 tons US)
ca. 110 km/h (= 68 mph) 180-200 km/h (= 110-125 mph) ca. 120 km/h (= 75 mph) 5000 m (= 16000 ft) 450 m (= 1500 ft) 400 m (= 1300 ft)
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