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United States' Curtiss P-40C / Tomahawk Mk IIB fighter1
| Curtiss P-40C1 | |
|---|---|
| Type | |
| Crew | |
| Engine (Type) | |
| Cylinders | |
| Cooling | |
| HP | |
| Propeller blades | |
| Dimensions | |
| Span | |
| Length | |
| Height | |
| Wing area | |
| Weight | |
| Empty | 5,812 lb1 2,636 kg1 |
| Loaded | 7,549 lb1 3,424 kg1 |
| Maximum load | 8,058 lb1 3,655 kg1 |
| Performance | |
| Speed @ 5,000 ' / 1,524 m |
|
| Speed @ 15,000' / 4,572 m |
345 mph1 555 kph1 |
| Speed @ 20,000' / 6,096 m |
|
| Cruising speed | 273 mph1 439 kph1 |
| Climb | 2,690'/minute1 820 m/minute1 |
| Climb to 15,000' / 4,572 m |
|
| Climb to 20,000' / 6,096 m |
|
| Service ceiling | 32,400'1 9,875 m1 |
| Range | 800 miles1 1,287 km1 |
| Range with drop tank | 1,230 miles1 1,979 km1 |
| Armament | |
| Nose | |
| Wings | |
| Bomb under fuselage | |
| OR | |
| Bomb under wings |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
