| Type | Aircraft | |
| Company | Curtiss Aeroplane and Motor Company | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
23.3
88.7
|
|
| Height (m) |
0.6
6.6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
126.3
925
|
|
| Wingspan (Beam) (m) |
0.1
32.9
95
|
|
| Weights | ||
| Empty weight (kg) |
8
14,700
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
20,411.7
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
435
28,165
|
at 4600 m |
| Сruise Speed (km/h) |
52
278
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
4,000
60,000
|
2 powerplants |
| Performance | ||
| Service ceiling (m) |
0.6
7,467.6
161,544
|
|
| Range (Ferry range) (km) |
4
5,069
40,700
|
at 278 km/h |
| Сombat radius (km) |
277
1,931
7,210
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
358.1
36,000
|
|
| Stat | ||
| Number built (qt) |
0
3,181
43,000
|
|
| Introduction | 1940 | |
| First flight | 26.03.1940 | |
