Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
6.1
88.7
|
|
Height (m) |
0.6
3.1
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
16.8
925
|
|
Wingspan (Beam) (m) |
0.1
11.3
95
|
|
Weights | ||
Empty weight (kg) |
8
1,170
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
1,540
575,000
|
|
Loaded weight (kg) |
5
1,540
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Ground Speed (km/h) |
96.6
357
1,500
|
|
Max. Speed (km/h) |
25
449
28,165
|
|
Сruise Speed (km/h) |
52
343
3,087
|
|
Power | ||
Total Power (hp) |
0.4
700
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
9,430
161,544
|
|
Range (Ferry range) (km) |
4
600
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
769
36,000
|
|
Time to altitude (min) |
0.6
6.5
105
|
to 5000 m |
Combat | ||
Guns (qt) |
1
2
18
|
1× 7.62 mm (0.30 in) ShKAS machine gun and 1× 20 mm (0.79 in) ShVAK cannon |
Stat | ||
Number built (qt) |
0
20
43,000
|
|
Introduction | 1933 | |
First flight | 27.05.1933 |