| Type | Aircraft | |
| Company | Joint Stock Company Tupolev | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
13.2
88.7
|
|
| Height (m) |
0.6
5.5
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
55.1
925
|
|
| Wingspan (Beam) (m) |
0.1
19.2
95
|
|
| Weights | ||
| Empty weight (kg) |
8
3,900
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
5,300
575,000
|
|
| Loaded weight (kg) |
5
5,300
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Speeds | ||
| Ground Speed (km/h) |
96.6
296
1,500
|
|
| Max. Speed (km/h) |
25
352
28,165
|
|
| Сruise Speed (km/h) |
52
321
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
1,072
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
2,038
60,000
|
2 powerplants 1019 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
9,170
161,544
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
526
36,000
|
|
| Combat | ||
| Guns (qt) |
1
3
18
|
1 moveable machine gun; 2 recoilless cannon |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1935 | |
| First flight | 01.02.1935 | |
