Curtiss XP-46

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XP-46
300px
Curtiss XP-46 (USAF photo)
Role Fighter
Manufacturer Curtiss-Wright Corporation
Designer Don R. Berlin
First flight 15 February 1941
Primary user United States Army Air Corps (intended)
Number built 2
Developed from Curtiss P-40
Developed into Curtiss XP-53

The Curtiss XP-46 was a 1940s United States 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 were to adversely affect performance.

Testing

In 1940 the British Purchasing Commission placed an order for the P-46 as a replacement for the P-40.[1]

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 was later cancelled.[1]

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.[2]

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 significance on its design.[3] NAA engineers had also made use of British research regarding the Meredith effect – the ability of an embedded ventral radiator to provide thrust.

Specifications (Curtiss XP-46A)

Data from Curtiss Aircraft 1907–1947[4]

General characteristics

Performance

  • Maximum speed: 355 mph (309 knots, 571 km/h) at 12,200 ft (3,720 m)
  • Range: 325 mi (283 nmi, 523 km)
  • Climb to 12,300 ft (3,750 m): 5 min

Armament

  • Guns:
    • 2 × .50 in (12.7 mm) synchronized machine guns in the forward fuselage
    • Provision for 8 × .30 in (7.62 mm) wing-mounted guns

See also

References

Notes

  1. 1.0 1.1 Engel, Leonard. "Half of Everything: An American's Survey of Orders Placed in the United States." Flight, 5 December 1940, p. 472.
  2. Berliner 2011, p. 18.
  3. Baugher, Joe. "North American NA-73." USAAC/USAAF/USAF Fighter and Pursuit Aircraft: North American P-51 Mustang, 29 August 1999. Retrieved: 10 August 2010.
  4. Bowers 1979, p. 436.

Bibliography

  • Berliner, Don. Surviving Fighter Aircraft of World War Two: Fighters. London: Pen & Sword Aviation, 2011. ISBN 978-1-8488-4265-6.
  • Bowers, Peter M. Curtiss Aircraft, 1907-1947. London: Putnam & Company Ltd., 1979. ISBN 0-370-10029-8.
  • Green, William. War Planes of the Second World War, Volume Four: Fighters. London: MacDonald & Co. (Publishers) Ltd., 1961 (Sixth impression 1969). ISBN 0-356-01448-7.
  • Green, William and Gordon Swanborough. WW2 Aircraft Fact Files: US Army Air Force Fighters, Part 1. London: Macdonald and Jane's Publishers Ltd., 1977. ISBN 0-356-08218-0.

External links