| Type | Aircraft | |
| Company | Joint Stock Company Tupolev | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
23.2
88.7
|
|
| Height (m) |
0.6
6.2
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
188.7
925
|
|
| Wingspan (Beam) (m) |
0.1
39.1
95
|
|
| Weights | ||
| Empty weight (kg) |
8
18,571
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
35,000
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
11
112
|
8 - 12 persons |
| Speeds | ||
| Ground Speed (km/h) |
96.6
347
1,500
|
|
| Max. Speed (km/h) |
25
443
28,165
|
on 6360 m |
| Power | ||
| Total Power (hp) |
0.4
5,360
60,000
|
|
| Performance | ||
| Service ceiling (m) |
0.6
9,300
161,544
|
|
| Range (Ferry range) (km) |
4
3,700
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
354
36,000
|
|
| Stat | ||
| Number built (qt) |
0
93
43,000
|
including 2 prototypes |
| Introduction | 1936 | |
| First flight | 27.12.1936 | |
