Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
24.4
88.7
|
|
Height (m) |
0.6
8.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
234.5
925
|
|
Wingspan (Beam) (m) |
0.1
41.8
95
|
|
Weights | ||
Empty weight (kg) |
8
11,200
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
19,300
575,000
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
|
Speeds | ||
Ground Speed (km/h) |
96.6
245
1,500
|
|
Max. Speed (km/h) |
25
212
28,165
|
at 3000 m |
Сruise Speed (km/h) |
52
182
3,087
|
|
Power | ||
Total Power (hp) |
0.4
2,820
60,000
|
4 powerplants 705 hp each |
Performance | ||
Service ceiling (m) |
0.6
4,800
161,544
|
|
Range (Ferry range) (km) |
4
2,000
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
75
36,000
|
|
Time to altitude (min) |
0.6
5
105
|
to 1000 m |
0.6
29
105
|
to 3000 m | |
Combat | ||
Guns (qt) |
1
8
18
|
5–8× 7.62 mm DA machine guns |
Bombs weight (kg) |
2
2,000
39,000
|
|
Stat | ||
Number built (qt) |
0
818
43,000
|
|
Introduction | 1934 | |
First flight | 22.12.1930 | |
Stop production | 1939 |