CURTISS P-40 TOMAHAWK

 

BRAND and MODEL
CURTISS P-40 TOMAHAWK
TYPE
Single-seat fighter
ORIGIN
United States of America
ENGINE
(Tomahawk I)
One 776 kw (1,040 hp) Allison V-1710-33 twelve-cylinder VEE liquid-cooled engine
SPECIFICATIONS
Wingspan: 11.36 m (37 ft 3½ in)
Length: 9.7 m (31 ft 8¾ in)
Height: 3.21 m (10 ft 7 in)
Max speed at 4,572 (15,000 ft): 575 km/h (357 mph)
Cruising speed: 446 km/h (277 mph)
Landing speed: 129 km/h (80 mph)
Initial rate of climb: 939 m/min (3,080 ft/min)
Service ceiling: 9,982 m (32,750 ft)
Range on internal fuel: 1,046 km (650 miles)
Max range: 2,253 km (1,400 miles)
Empty weight: 2,439 kg (5,376 lb)
Normal loaded weight: 3,079 kg (6,787 lb)
Max loaded weight: 3,273 kg (7,215 lb)
PHOTO
Airliners.net:Source of phothograph