| Type | Aircraft | |
| Company | Curtiss Aeroplane and Motor Company | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
39
88.7
|
|
| Height (m) |
0.6
3.7
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
14.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
5,564.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
8,628.2
575,000
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
531
28,165
|
at 5200 m |
| Power | ||
| Total Power (hp) |
0.4
2,500
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
8,016.2
161,544
|
|
| Range (Ferry range) (km) |
4
2,108
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
9.6
36,000
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
20 mm (0.79 in) cannon (wing) |
| Bombs weight (kg) |
2
907
39,000
|
|
| Stat | ||
| Number built (qt) |
0
9
43,000
|
|
| First flight | 01.03.1945 | |
