Bell P-76

Length
9.7 m
Flat Wing Span
10.9 m
Flat Wing Area
21.9 m²
Max Speed
620 km/h
Number of Engines
1
First Flight
1942-01-01
Number Built
0
Maximum Take-Off Weight
4.05 t (paragliders: kg)

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg))
Bell P-76 4.05

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All data (19 fields)
Name
Bell P-76
Manufacturer
Bell Aircraft Corporation
Description
The Bell P-76 was the proposed designation for a production model derivative of the XP-39E, a single-engine American fighter aircraft prototype of World War II.
First Flight
1942-01-01
Designer
Bell Aircraft Corporation
Type
Fighter aircraft
Length (m)
9.7
Cockpit Crew
1
Max Speed (km/h)
620
Rate of Climb (m/s)
11
Armament
; 1× 37 mm (1.46 in) Oldsmobile T9 cannon, 30 rounds; 2× 0.50 in (12.7 mm) M2 Browning machine guns, 200 rounds per gun; 4× 0.30 in (7.62 mm) M1919 machine guns, 1,000 rounds per gun; 500 lb (227 kg) externally
Number Built
0
Powerplant Description
1 × Continental I-1430-1, 1600 kW (2146 hp) each
Primary Users
United States Army Air Forces
Status
Did not enter mass-production
Wikipedia Article (URL)
en.wikipedia.org/wiki/Bell_P-76
Flat Wing Span (m)
10.9
Flat Wing Area (m²)
21.9
Number of Engines
1