CURTISS HAWK 75A

 

BRAND and MODEL
CURTISS HAWK 75A
TYPE
Single-seat fighter
ORIGIN
United States of America
ENGINE
(Hawk 75O)
One 653 kw (875 hp) Wright Cyclone GR-1820-G3 nine-cylinder air-cooled radial engine
SPECIFICATIONS
Wingspan: 11.4 m (37 ft 4 in)
Length: 8.68 m (28 ft 6 in)
Height: 2.86 m (9 ft 4 in)
Wing area: 21.92 m² (236 sq ft)
Max speed at sea level: 384 km/h (239 mph)
Max speed at 3,260 m (10,700 ft): 451 km/h (280 mph)
Normal cruising speed at 3,260 m (10,700 ft): 386 km/h (240 mph)
Initial rate of climb: 713 m/min (2,340 ft/min)
Time to 7,010 m (23,000 ft): 12 mins 52 secs
Service ceiling: 9,690 m (31,800 ft)
Normal range: 880 km (547 miles)
Max range: 1,947 km (1,210 miles)
Empty weight: 1,803 kg (3,975 lb)
Loaded weight: 2,346 kg (5,172 lb)
Max overload weight: 2,911 kg (6,418 lb)

PHOTO
Flickr:Source of phothograph