Flat Wing Area
40.0412 m²
Maximum Take-Off Weight
12.4738 t (paragliders: kg)
Total Fuel Capacity
4368.365
Maximum Range
2784.165 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Bell XP-83 |
12.4738 |
4368.365 |
2784.165 |
Similar airplanes
All data (21 fields)
- Name
- Bell XP-83
- Manufacturer
- Bell Aircraft Corporation
- Description
- The Bell XP-83 (later redesignated XF-83) was a United States prototype jet escort fighter designed by Bell Aircraft during World War II.
- First Flight
- 1945-02-25
- Designer
- Bell Aircraft Corporation
- Type
- Escort fighter
- Length (m)
- 13.4112
- Height (m)
- 4.572
- Cockpit Crew
- 1
- Max Speed (km/h)
- 840.0776
- Max Ceiling (m)
- 13716
- Rate of Climb (m/s)
- 28.702
- Armament
- ; 6 × .50 in (12.7 mm) M2 machine guns or; 6 × .60 in (15.2 mm) T17E3 machine guns (prototypes) or; 4 × 20 mm (0.79 in) Hispano cannons or; 1 × 37 mm (1.46 in) cannon in the nose; 2 × 1000 lb bombs
- Number Built
- 2
- Powerplant Description
- 2 × General Electric XJ33-GE-5 centrifugal-flow compressor turbojet engines
- Primary Users
- United States Army Air Forces (intended)
- Status
- Project cancelled 1947
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Bell_XP-83
- Flat Wing Span (m)
- 16.1544
- Flat Wing Area (m²)
- 40.0412
- Number of Engines
- 2