| Type | Aircraft | |
| Company | Joint Stock Company Tupolev | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
35.4
88.7
|
|
| Height (m) |
0.6
9.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
161.7
925
|
|
| Wingspan (Beam) (m) |
0.1
44.3
95
|
|
| Weights | ||
| Empty weight (kg) |
8
38,290
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
60,000
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
7
112
|
or 8 |
| Capacity passengers (per.) |
1
72
400
|
Up to 72 |
| Speeds | ||
| Max. Speed (km/h) |
25
568
28,165
|
at 9000 m |
| Сruise Speed (km/h) |
52
563
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
9,600
60,000
|
4 powerplants 2400 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
11,000
161,544
|
|
| Range (Ferry range) (km) |
4
4,900
40,700
|
|
| Takeoff roll (m) |
20
670
3,200
|
|
| Landing roll (m) |
20
600
2,570
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
21.2
105
|
to 5000 m |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1946 | |
| First flight | 27.11.1946 | |
