Flat Wing Area
398.0895 m²
Cruise Speed
217.2614 km/h
Maximum Take-Off Weight
73.482 t (paragliders: kg)
Total Fuel Capacity
39179.01
Maximum Range
8368.589 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Douglas XB-19 |
73.482 |
39179.01 |
8368.589 |
Similar airplanes
All data (24 fields)
- Name
- Douglas XB-19
- Manufacturer
- 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.
- First Flight
- 1941-06-27
- Service End
- 1946-08-17
- Designer
- Douglas Aircraft Corporation
- Type
- Heavy bomber
- Length (m)
- 40.2336
- Height (m)
- 12.8016
- Cockpit Crew
- 16
- 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
- National Origin
- United States of America
- Number Built
- 1
- Powerplant Description
- 4 × Wright R-3350-5 Duplex Cyclone 18-cylinder air-cooled radial piston engines, 1491 kW (2000 hp) each
- Primary Users
- United States Army Air Corps
- Status
- Scrapped
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Douglas_XB-19
- Flat Wing Span (m)
- 64.6176
- Flat Wing Area (m²)
- 398.0895
- Number of Engines
- 4