CONSOLIDATED B-24 LIBERATOR

 

BRAND and MODEL
CONSOLIDATED B-24 LIBERATOR
TYPE
Long-range heavy bomber
ORIGIN
United States of America
ENGINE
(B-24J)
Four 895 kw (1,200 hp) Pratt & Whitney R-1830-65 fourteen-cylinder two-row supercharged aircooled radial engines
SPECIFICATIONS
Wingspan: 33.52 m (110 ft)
Length: 20.48 m (67 ft 2 in)
Height: 5.48 m (18 ft)
Wing area: 97.36 m² (1,048 sq ft)
Max speed at 9,144 m (30,000 ft): 483 km/h (300 mph)
Max continuous speed at 7,620 m (25,000 ft): 447 k/h (278 mph)
Normal cruising speed at 7,620 m (25,000 ft): 382 km/h (237 mph)
Initial rate of climb: 312 m/min (1,025 ft/min)
Service ceiling: 8,534 m (28,000 ft)
Range with 2,268 kg (5,000 lb) bomb load at 7,620 m (25,000 ft): with 8,946.5 litres (1,968 Imp gals)
fuel 2,736 km (1,700 miles)
Landing speed: 169 km/h (105 mph)
Empty weight: 17,237 kg (38,000 lb)
Loaded weight: 25,401 kg (56,000 lb)
Max overload weight: 32,296 kg (71,200 lb)
PHOTO
pixels.com:Source of phothograph