| Company | Curtiss Aeroplane and Motor Company | |
| Scheme | Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
13.4
88.7
|
|
| Height (m) |
0.6
4.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
400
925
|
|
| Wingspan (Beam) (m) |
0.1
14.6
95
|
|
| Weights | ||
| Empty weight (kg) |
8
5,739
276,800
|
|
| Loaded weight (kg) |
5
7,543
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
755
28,165
|
|
| Power | ||
| Total Power (hp) |
0.4
2,100
60,000
|
|
| Thrust (kN) |
1.5
12.3
1,914
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
25.5
36,000
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
wing-mounted 20 mm (.79 in) cannon |
| Stat | ||
| Number built (qt) |
0
3
43,000
|
|
| First flight | 27.02.1945 | |
