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Junkers Ju 252
Specifications

Type: Transport
Origin: Junkers Flugzeug und Motorenwerke AG
Models: V1 to V15 and A-1
Production: N/A
First Flight: October 1941

Powerplants:
  • Ju 252A-1:
    • Model: Junkers Jumo 211F
    • Type: Inverted V12 liquid cooled
    • Number: Three
    • Horsepower: 1,350 hp
    • Propellers: 3-bladed constant-speed propellers

Dimensions:
  • Wing span: 34.09m (111 ft. 10¼ in.)
  • Wing Surface Area: 122.6 m2 (1,320 sq ft)
  • Length: 25.10m (82 ft. 4¼ in.)
  • Height: 5.75m (18 ft. 10½ in.)

Weights:
  • Empty weight: 13,127 kg (28,940 lb)
  • Gross weight: 22,257 kg (49,068 lb)
  • Max takeoff weight: 24,050 kg (53,021 lb)

Performance:
  • Maximum speed: 438 km/h (272 mph, 237 kn) at 5,800 m (19,029 ft)
  • Cruise speed: 335 km/h (208 mph, 181 kn) (econ. cruise)
  • Range:
    • 3,981 km (2,474 mi, 2,150 nmi) with maximum payload
    • 6,600 km (4,100 mi; 3,600 nmi) with 2,000 kg (4,409 lb) payload
  • Service ceiling: 6,300 m (20,700 ft)
  • Rate of climb: 12.5 m/s (2,460 ft/min)

Armament:
  • 1 x MG 131 in EDL 131 turret mounted dorsally
  • 2 x MG 15 in beam windows.

Sources:
Gunston, Bill & Wood, Tony - Hitler's Luftwaffe, 1977, Salamander Books Ltd., London
Wikipedia: Junkers Ju 252
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