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Curtiss P-60

Military Aircraft

The Curtiss P-60 was an American single-seat, single-engine, low-wing fighter developed by Curtiss-Wright in the early 1940s as the successor to the P-40 Warhawk. Work began with the XP-53, which became the XP-60 and then a long run of prototypes, among them the XP-60A, XP-60C and XP-60E, that tried different engines and propellers, including the Packard-built Merlin, the Allison V-1710 and the Pratt and Whitney R-2800 with contra-rotating propellers. The design ended up looking little like the P-40. Laminar-flow wing finish problems, drag and engine output held back the performance, and the Army Air Forces turned Curtiss toward building P-47 Thunderbolts instead. Large production orders were cancelled, only two pre-production YP-60 aircraft were ever built, and no version entered service.

Facts
Year
1941 1
Engine Class
Piston 1
Status
Cancelled 1
Power (kW)
1491 1
Top Speed (km/h)
666 1
Mass (kg)
3901 1
Maximum Mass (kg)
5368.3 1
Engine
Pratt & Whitney R-2800-53 18-cylinder air-cooled radial piston engine (XP-60C) 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Curtiss P-60 (Wikipedia)

Of Make

Source Curtiss P-60 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Curtiss P-60 (Wikipedia)Lead, maker
Quote, Lead, maker
The Curtiss P-60 was a 1940s American single-engine single-seat, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to its P-40.

Originated In

Also in Geography Atlas: where this subject originated.

Source Curtiss P-60 (Wikipedia)Lead, origin
Quote, Lead, origin
The Curtiss P-60 was a 1940s American single-engine single-seat, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to its P-40.
Sources
1. Curtiss P-60 (Wikipedia)
  • Lead, maker
    The Curtiss P-60 was a 1940s American single-engine single-seat, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to its P-40.
  • Specifications (XP-60C), powerplant
    Powerplant: 1 × Pratt & Whitney R-2800-53 18-cylinder air-cooled radial piston engine, 2,000 hp (1,500 kW)
  • Design and development, first flight
    This aircraft first flew on 18 September 1941 with a British Merlin 28 engine.
  • Design and development, production cancelled
    In February 1942, the production of P-60As was cancelled so that Curtiss could build a further 1,400 P-40s
  • Specifications (XP-60C), empty weight
    Empty weight: 8,600 lb (3,901 kg)
  • Specifications (XP-60C), gross weight
    Gross weight: 11,835 lb (5,368 kg)
  • Specifications (XP-60C), maximum speed
    Maximum speed: 414 mph (666 km/h, 360 kn) at 20,350 ft (6,200 m)
  • Lead, origin
    The Curtiss P-60 was a 1940s American single-engine single-seat, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to its P-40.
  • In Group: Propeller-Driven Fighters, Lead, role
    The Curtiss P-60 was a 1940s American single-engine single-seat, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to its P-40.
  • Exemplifies: Aviation, Lead, aircraft
    The Curtiss P-60 was a 1940s American single-engine single-seat, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to its P-40.
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