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 |