North American B-25 Mitchell
Flat Wing Area
57.4141 m²
Cruise Speed
370.1491 km/h
Entry Into service
1941-01-01
Maximum Take-Off Weight
15.8757 t (paragliders: kg)
Maximum Range
2172.615 km
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All data (23 fields)
- Name
- North American B-25 Mitchell
- Manufacturer
- North American Aviation
- Description
- The North American B-25 Mitchell is a twin-engined medium bomber designed and produced by the American aircraft manufacturer North American Aviation.
- ICAO Code
- B25
- First Flight
- 1940-08-19
- Entry Into service
- 1941-01-01
- Service End
- 1974-01-01
- Designer
- North American Aviation
- Length (m)
- 15.8496
- Height (m)
- 4.8768
- Max Speed (km/h)
- 437.7416
- Cruise Speed (km/h)
- 370.1491
- Max Ceiling (m)
- 7376.16
- Armament
- 12–18 × .50 in (12.7 mm) machine guns and 75 mm (2.95 in) T13E1 cannon; 3,000 lb (1,360 kg) bombs; racks for eight 5 in high velocity aircraft rockets (HVAR); 2,000 lb (900 kg) ventral shackles to hold one external Mark 13 torpedo
- National Origin
- United States of America
- Number Built
- 9816
- Powerplant Description
- 2 × Wright R-2600-92 Twin Cyclone 14-cylinder two-row air-cooled radial piston engines, 1268 kW (1700 hp) each
- Primary Users
- United States Army Air Forces, Royal Air Force , Soviet Air Force , United States Marine Corps
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/North_American_B-25_Mitchell
- Flat Wing Span (m)
- 20.4216
- Flat Wing Area (m²)
- 57.4141
- Wake Category
- M
- Number of Engines
- 2