Flat Wing Area
104.0514 m²
Cruise Speed
305.7754 km/h
Maximum Take-Off Weight
18.1437 t (paragliders: kg)
Maximum Range
3154.314 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
North American XB-21 |
18.1437 |
3154.314 |
Similar airplanes
All data (21 fields)
- Name
- North American XB-21
- Manufacturer
- North American Aviation
- Description
- The North American XB-21 (manufacturer's model designation NA-21) and sometimes referred to by the name "Dragon", was a prototype bomber aircraft developed by North American Aviation in the late 1930s, for evaluation by the United States Army Air Corps.
- First Flight
- 1936-12-22
- Designer
- North American Aviation
- Type
- Medium bomber
- Length (m)
- 18.5928
- Height (m)
- 4.2672
- Max Speed (km/h)
- 354.0557
- Cruise Speed (km/h)
- 305.7754
- Max Ceiling (m)
- 7620
- Armament
- Five .30-calibre machine guns, mounted in single turrets in the nose and dorsal positions, and single manually operated mounts in the waist and ventral positions.; Up to 10000 lb in an internal bay.
- National Origin
- United States of America
- Number Built
- 1
- Powerplant Description
- 2 × Pratt & Whitney R-2180-A Twin Hornet turbosupercharged radial engines, 895 kW (1200 hp) each
- Primary Users
- United States Army Air Corps
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/North_American_XB-21
- Flat Wing Span (m)
- 28.956
- Flat Wing Area (m²)
- 104.0514
- Aircraft Engine
- Pratt & Whitney R-2180-A Twin Hornet
- Number of Engines
- 2