Curtiss P-60

· Military designations USAAS/USAAF/USAF
Airplanes
Length
10.0584 m
Flat Wing Span
12.4968 m
Height
3.048 m
Flat Wing Area
25.5483 m²
Max Speed
666.2684 km/h
Max Ceiling
10668 m
Number of Engines
1
First Flight
1941-09-18
Number Built
1
Maximum Range
506.9434 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Curtiss P-60 506.9434

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All data (23 fields)
Name
Curtiss P-60
Manufacturer
Military designations USAAS/USAAF/USAF
Description
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.
First Flight
1941-09-18
Production End
1944-01-01
Service End
1944-12-22
Designer
Military designations USAAS/USAAF/USAF
Type
Fighter aircraft
Length (m)
10.0584
Height (m)
3.048
Cockpit Crew
1
Max Speed (km/h)
666.2684
Max Ceiling (m)
10668
Rate of Climb (m/s)
19.7612
Armament
4 × 0.50 in M2 Browning machine guns
Number Built
1
Powerplant Description
1 × Pratt & Whitney R-2800-53 18-cylinder air-cooled radial piston engine, 1491 kW (2000 hp) each
Primary Users
United States Army Air Forces
Status
Canceled
Wikipedia Article (URL)
en.wikipedia.org/wiki/Curtiss_P-60
Flat Wing Span (m)
12.4968
Flat Wing Area (m²)
25.5483
Number of Engines
1