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Curtiss P-40 Warhawk Specifications
Curtiss P-40 Warhawk
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| Data for Aircraft | Curtiss P-40 Warhawk |
| Year Introduced | 1938 |
| Number Built | 13,738 |
| Rotor Diameter | |
| Wingspan | 37.33 ft (11.38 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 12.33 ft (3.76 m) |
| Wing Area | 235.94 ft² (21.92 m²) |
| Wing Loading | 35.1 lb/ft² (171.5 kg/m²) |
| Length | 31.67 ft (9.66 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Allison V-1710-39, 1,150 hp (858 kW) |
| Country of Origin | USA |
| Empty Weight | 6,350 lb (2,880 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 8,810 lb (4,000 kg) |
| Useful Load | 2460 lb |
| Seats | 1 |
| Crew | 1 |
| Power Loading | 0.14 hp/lb (230 W/kg) |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | |
| Oil Capacity |
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