• Source: Curtiss XP-46

The Curtiss XP-46 was a 1940s American prototype fighter aircraft. It was a development of the Curtiss-Wright Corporation in an effort to introduce the best features found in European fighter aircraft in 1939 into a fighter aircraft which could succeed the Curtiss P-40, then in production.




Design and development


A United States Army Air Corps (USAAC) specification based upon a Curtiss proposal was the basis for an order placed in September 1939 for the XP-46. The requirements called for a single-engine, low-wing aircraft, slightly smaller than the P-40, and with a wide-track, inward-retracting landing gear. The selected powerplant was a 1,150 hp (858 kW) Allison V-1710-39 V-12 engine. The planned armament included two .50 in (12.7 mm) synchronized machine guns in the forward fuselage and provisions for eight .30 in (7.62 mm) wing-mounted guns. The USAAC later added requirements for self-sealing fuel tanks and 65 lb (29 kg) of armor, the weights of which adversely affected performance.




Testing


In 1940 the British Purchasing Commission placed an order for the P-46 as a replacement for the P-40, the British service name 'Kittyhawk' was allocated by the Air Ministry in anticipation of receiving the aircraft.
However, the USAAC asked Curtiss in July 1940 – while the XP-46 prototypes were under construction – to prioritize an upgraded P-40, featuring the engine intended for the XP-46. This would also avoid disruptions to the production line caused by any switch to a new airframe. The British order for the P-46 was later cancelled, and the 'Kittyhawk' name subsequently applied to the upgraded P-40.
Two prototypes, designated XP-46A, were nevertheless delivered to the USAAC; the first flight occurred on 15 February 1941. The type's performance during trials was found to be inferior to the then-contemporary P-40D. As the P-46 offered no significant improvement on the P-40, the program was cancelled.
A myth claims that work on the XP-46 was the basis of the North American NA-73X – the prototype P-51 Mustang. While North American Aviation (NAA) purchased technical aerodynamic data on the P-40 and XP-46 from Curtiss for $56,000, and there are certain design similarities in the radiator/oil-cooler configuration of the two types, North American had already made significant progress on its design.




Specifications (Curtiss XP-46A)



Data from Curtiss Aircraft 1907–1947General characteristics
Crew: 1
Length: 30 ft 2 in (9.19 m)
Wingspan: 34 ft 3.75 in (10.4585 m)
Height: 10 ft 1 in (3.07 m)
Wing area: 208 sq ft (19.3 m2)
Airfoil: root: NACA 23016.5; tip: NACA 23009
Empty weight: 5,625 lb (2,551 kg)
Gross weight: 7,665 lb (3,477 kg)
Powerplant: 1 × Allison V-1710-39 V-12 liquid-cooled piston engine, 1,150 hp (860 kW)
Propellers: 3-bladed constant-speed propeller
Performance

Maximum speed: 355 mph (571 km/h, 308 kn) at 12,200 ft (3,700 m)
Range: 325 mi (523 km, 282 nmi)
Time to altitude: 12,300 ft (3,700 m) in 5 minutes
Armament

Guns:
2 × 0.50 in (13 mm) synchronized machine guns in the forward fuselage
Provision for 8 × 0.30 in (7.6 mm) wing-mounted guns




See also


Curtiss P-40
Curtiss XP-42 - an earlier design also intended to replace the P-40, but not put into production
North American P-51 Mustang
Curtiss P-60 – a series of designs developed from the XP-46




References






= Notes

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= Bibliography

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External links



Curtiss XP-46

Kata Kunci Pencarian:

• Curtiss P-40 Warhawk
• Curtiss XP-46
• Curtiss P-60
• Curtiss XP-42
• Curtiss P-6 Hawk
• Curtiss-Wright XP-55 Ascender
• Curtiss YP-37
• Curtiss P-36 Hawk
• Curtiss P-40 Warhawk variants
• Curtiss P-1 Hawk
• List of aircraft of the United States during World War II