| Type | Aircraft | |
| Company | Curtiss Aeroplane and Motor Company | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.1
88.7
|
|
| Height (m) |
0.6
4.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
26.0
925
|
|
| Wingspan (Beam) (m) |
0.1
12.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
2,866.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
4,082
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
504
28,165
|
at 8700 m |
| Сruise Speed (km/h) |
52
210
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
1,350
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
11,369.0
161,544
|
|
| Range (Ferry range) (km) |
4
1,006
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
762
36,000
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
.50 M2 Browning machine guns |
| Bombs (qt) |
1
2
250
|
150 kg bombs |
| Stat | ||
| Number built (qt) |
0
577
43,000
|
|
| Introduction | 1944 | |
| First flight | 16.02.1944 | |
| Stop production | 1949 | |
