Type: Heavy Bomber. Origin: Armstrong Whitworth Models: Whitley I to VIII Crew: Five First Flight: Prototype: March 17, 1936 Mark V: December 1938 Service Delivery: Mk. I: January 1937 Service Delivery: Mk. V: August 1939 Production Termination: June 1943 Number Produced: 1,737 Mark V: 1,466 Gr.VIII: 146 Engine: Whitley Mk. V Model: Rolls-Royce Merlin X Type: 12-Cylinder liquid cooled vee Number: Two Horsepower: 1,145 hp Dimensions: Whitley Mk. V Wing span: 84 ft. (25.6m) Length: 70 ft. 6 in. (21.5m) Height: 15 ft. (4.57m) Wing Surface Area: N/A |
Weights: Whitley Mk. V Empty: 19,330 lb. (8768 kg) Loaded: 33,500 lb. (15,196 kg) Performance: Whitley Mk. V Maximum Speed: 222 mph (357 km/h) Cruising Speed: about 185 mph (297 km/h) Initial Climb: 800 ft/min (244 m/min) Service Ceiling: 17,600-21,000 ft. (5400-6400m) Range with 3,000 lb. (1361 kg.) bomb load: 1,650 miles (2650 km) Armament: Whitley Mk. V One .303 in. Vickers K in nose turret. Four .303 in. Vickers K in tail turret. Payload: Whitley Mk. V 7,000 lb (3175 kg. of bombs in cells in fuselage and inner wing. |
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