Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
15.1
88.7
|
|
Wings | ||
Wing area (m2) |
1.1
80
925
|
|
Wingspan (Beam) (m) |
0.1
23.2
95
|
|
Wing loading (kg/m2) |
3.1
81
829
|
|
Weights | ||
Empty weight (kg) |
8
3,856
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
6,472
575,000
|
|
Loaded weight (kg) |
5
6,472
242,500
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
|
Speeds | ||
Ground Speed (km/h) |
96.6
260
1,500
|
|
Max. Speed (km/h) |
25
220
28,165
|
|
Сruise Speed (km/h) |
52
205
3,087
|
|
Power | ||
Power/mass (hp/kg) |
0.0
0.2
22.1
|
|
Total Power (hp) |
0.4
1,440
60,000
|
2 powerplants |
Performance | ||
Service ceiling (m) |
0.6
6,050
161,544
|
|
Range (Ferry range) (km) |
4
1,680
40,700
|
|
Takeoff roll (m) |
20
160
3,200
|
|
Landing roll (m) |
20
180
2,570
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
167
36,000
|
|
Combat | ||
Guns (qt) |
1
1
18
|
|
Stat | ||
Number built (qt) |
0
411
43,000
|
|
Introduction | 11.09.1929 | |
First flight | 01.05.1930 | |
Stop production | 1934 |