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United States' Curtiss P-40D / Kittyhawk Mk I fighter1
| Curtiss P-40D1 | |
|---|---|
| Type | Fighter bomber1 |
| Crew | 11 |
| Engine (Type) | Allison V-1710-391 |
| Cylinders | V 121 |
| Cooling | |
| HP | 1,1501 |
| Propeller blades | 31 |
| Dimensions | |
| Span | 37' 3.5"1 11.37 m1 |
| Length | 31' 9"1 9.68 m1 |
| Height | 12' 4"1 3.76 m1 |
| Wing area | |
| Weight | |
| Empty | |
| Loaded | |
| Maximum load | |
| Performance | |
| Speed @ 5,000 ' / 1,524 m |
|
| Speed @ 15,000' / 4,572 m |
|
| Speed @ 20,000' / 6,096 m |
|
| Cruising speed | |
| Climb | |
| Climb to 15,000' / 4,572 m |
|
| Climb to 20,000' / 6,096 m |
|
| Service ceiling | |
| Range | |
| Range with drop tank | |
| Armament | |
| Nose | |
| Wings | 4: 0.5" MG1 |
| Bomb under fuselage | |
| OR | |
| Bomb under wings |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
