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 |