Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
54.1
88.7
|
|
Height (m) |
0.6
15.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
311.1
925
|
|
Wingspan (Beam) (m) |
0.1
51.1
95
|
|
Weights | ||
Empty weight (kg) |
8
88,200
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
179,000
575,000
|
|
Capacity | ||
Crew (per.) |
1
5
112
|
|
Useful load (kg) |
26.4
30,000.6
90,700
|
|
Payload (kg) |
23
30,000.6
122,470
|
|
Capacity passengers (per.) |
1
220
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
870
28,165
|
at 7100 m |
Сruise Speed (km/h) |
52
770
3,087
|
|
Power | ||
Total Power (hp) |
0.4
60,000
60,000
|
4 powerplants 15000 hp each |
Performance | ||
Service ceiling (m) |
0.6
12,000
161,544
|
|
Range (Ferry range) (km) |
4
9,720
40,700
|
loaded with 15000 kg |
Takeoff roll (m) |
20
1,600
3,200
|
|
Landing roll (m) |
20
1,550
2,570
|
|
Stat | ||
Number built (qt) |
0
32
43,000
|
|
Introduction | 1957 | |
First flight | 15.11.1957 | |
Stop production | 1991 |