| Type | Aircraft | |
| Company | Joint Stock Company Tupolev | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
47.9
88.7
|
|
| Height (m) |
0.6
11.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
201.5
925
|
|
| Wingspan (Beam) (m) |
0.1
37.6
95
|
|
| Weights | ||
| Empty weight (kg) |
8
50,775
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
100,000
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
or 3 |
| Capacity passengers (per.) |
1
180
400
|
|
| Speeds | ||
| Сruise Speed (km/h) |
52
950
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
47,000
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
270
1,914
|
3 powerplants 90 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
12,000
161,544
|
|
| Range (Ferry range) (km) |
4
3,900
40,700
|
with max fuel |
|
4
2,500
40,700
|
fully loaded | |
| Stat | ||
| Number built (qt) |
0
1,026
43,000
|
|
| Introduction | 1968 | |
| First flight | 04.10.1968 | |
