Flat Wing Area
19.7883 m²
Entry Into service
1941-01-01
Maximum Take-Off Weight
3.8102 t (paragliders: kg)
Maximum Range
844.9056 km
Pictures
No pictures yet for this family.
Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Bell P-39 Airacobra |
3.8102 |
844.9056 |
Similar airplanes
All data (25 fields)
- Name
- Bell P-39 Airacobra
- Manufacturer
- Bell Aircraft Corporation
- Description
- The Bell P-39 Airacobra is a fighter produced by Bell Aircraft for the United States Army Air Forces during World War II.
- ICAO Code
- P39
- First Flight
- 1938-04-06
- Entry Into service
- 1941-01-01
- Designer
- Bell Aircraft Corporation
- Type
- Fighter
- Length (m)
- 9.144
- Height (m)
- 3.6576
- Max Speed (km/h)
- 626.0348
- Min Speed (km/h)
- 152.8877
- Max Ceiling (m)
- 10668
- Rate of Climb (m/s)
- 19.3294
- Armament
- :* 1 × 37 mm M4 cannon firing through the propeller hub (compare engine gun) :* 2 × .50 caliber synchronized Browning M2 machine guns, nose-mounted :* 2 × .50 caliber Browning M2 machine guns on each wing; Up to 500 lb of bombs under wings and belly
- National Origin
- United States of America
- Number Built
- 9588
- Powerplant Description
- 1 × Allison V-1710-85 V-12 liquid-cooled piston engine, 895 kW (1200 hp) each
- Primary Users
- United States Army Air Forces, Soviet Air Force, Royal Air Force
- Status
- Retired
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Bell_P-39_Airacobra
- Flat Wing Span (m)
- 10.3632
- Flat Wing Area (m²)
- 19.7883
- Wake Category
- L
- Number of Engines
- 1