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Douglas XB-19 ✕ Douglas 423 ✕
Manufacturer Douglas Aircraft Corporation Douglas Aircraft Corporation
Description The Douglas XB-19 was a four-engined, piston-driven heavy bomber produced by the Douglas Aircraft Company for the United States Army Air Forces (USAAF) during the early 1940s. The Douglas Model 423 was a bomber aircraft design developed by American aircraft manufacturer Douglas to compete with the Convair B-36 design for a major U.S.
First Flight 1941-06-27
Service End 1946-08-17
Designer Douglas Aircraft Corporation Douglas Aircraft Corporation
Type Heavy bomber
Length (m) 40.2336 35.6616
Height (m) 12.8016 12.8016
Cockpit Crew 16 8
Max Speed (km/h) 360.4931
Cruise Speed (km/h) 217.2614
Max Ceiling (m) 7010.4
Rate of Climb (m/s) 3.302
Armament :*5 × 0.5 in M2 Browning machine guns :*6 × 0.3 in M1919 Browning machine guns :*2 × 37 mm M4 autocannon; 18700 lb internal; maximum bomb load of 37100 lb including external racks with reduced fuel load ; 6× 0.50 in machine guns in remote ventral and dorsal turrets; 2× 37 mm cannon; ; 25000 lb of bombs
National Origin United States of America
Number Built 1 0
Powerplant Description 4 × Wright R-3350-5 Duplex Cyclone 18-cylinder air-cooled radial piston engines, 1491 kW (2000 hp) each 4 × Pratt & Whitney R-4360 Wasp Major 28-cylinder air-cooled radial piston engines, 2237 kW (3000 hp) each
Primary Users United States Army Air Corps United States Army Air Force
Status Scrapped Design only
Wikipedia Article (URL) en.wikipedia.org/wiki/Douglas_XB-19 en.wikipedia.org/wiki/Douglas_423
Flat Wing Span (m) 64.6176 63.0936
Flat Wing Area (m²) 398.0895 306.58
Aircraft Engine Pratt & Whitney R-4360 Wasp Major
Number of Engines 4 4