|Manufacturer||Bell Aircraft Corporation|
|Status||Did not enter mass-production|
|Primary user||United States Army Air Forces|
|Number built||0 (3 prototypes built as XP-39Es)|
|Developed from||Bell P-39 Airacobra|
Design and development
On 26 February 1941 the United States Army Air Corps (USAAC) placed a contract with Bell allowing for the purchase of two XP-39Es (41-19501 and 41-19502) which were envisaged to be a major improvement on the P-39D series. Because of the number of changes proposed the production model was to be called the Bell P-76.
The Bell P-76 was proposed to address the poor high-altitude performance of the P-39 Airacobra by incorporating a new and thicker wing with a symmetrical airfoil; the section chosen was NACA 0018 at the wing-root tapering to an NACA 23009 at the tip. Although the new wing has often been referred to as a laminar flow type, this was not the case. The wing span was increased to 35 ft 10 in (10.9 m) and the area to 236 ft² (21.9 m²), the thicker wing allowing an increase in the fuel capacity to 150 US gallons (568 l).
Design of a new Allison V-1710-E9 was also underway. This version, which had the military designation of V-1710-47, used a two-stage mechanical supercharger to increase the engine power at altitude. However, this engine went through so many design changes that it ended up being almost identical to the later V-1710-93 which was fitted in the XP-63A.
Another change was the engine bay was modified to accept a more powerful engine in lieu of the V-1710. Its origins lie in the 1941 project to equip three P-39D (41-19501, 41-19502 and 42-7164) with the Continental V-1430-1 liquid-cooled supercharged engine. The resultant XP-39E had a symmetrical airfoil wing with square wingtips, an elongated fuselage to accommodate the larger engine, and revised air intakes and radiators. The three prototypes each had a different tailfin. Since the Continental engine was not available at rollout, the prototypes flew with Allison V-1710-47 engines. In 1942, the XP-39E was redesignated P-76. Although 4,000 aircraft were initially ordered, the order was cancelled to permit the Bell factory to manufacture B-29 Superfortress bomber aircraft under license from Boeing. Many of the lessons learned in the P-76 were implemented in the subsequent Bell P-63 Kingcobra.
- Crew: 1
- Length: 31 ft 11 in (9.7 m)
- Wingspan: 35 ft 10 in (10.9 m)
- Height: ft in (m)
- Wing area: 236 ft² (21.9 m²)
- Empty weight: 6,936 lb (3,150 kg)
- Max. takeoff weight: 8,918 lb (4,050 kg)
- Powerplant: 1 × Continental I-1430-1, 2,100 hp (1,600 kW)
- Maximum speed: 386 mph (335 knots, 620 km/h) at 21,680 ft (6,600 m)
- Rate of climb: 2,150 ft/min (11 m/s)
- Bombs: 500 lb (227 kg) externally
- Bowers, Peter M. "Airborne Cobra Pt.II". Airpower magazine, Vol.9, No.1, January 1979.