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 |