| Type | Aircraft | |
| Company | Joint Stock Company Tupolev | |
| Scheme | Concept Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
46.2
88.7
|
|
| Height (m) |
0.6
13.9
50.1
|
in tail |
| Wings | ||
| Wing area (m2) |
1.1
184.2
925
|
|
| Wingspan (Beam) (m) |
0.1
41.8
95
|
|
| Weights | ||
| Empty weight (kg) |
8
58,600
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
110,000
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
or 2 |
| Speeds | ||
| Сruise Speed (km/h) |
52
850
3,087
|
810 to 850 km/h |
| Fuel | ||
| Fuel Capacity (l) |
23
34,000
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
384
1,914
|
2 powerolants 192 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
10,800
161,544
|
|
| Range (Ferry range) (km) |
4
4,800
40,700
|
4100 - 5800 km with max payload |
| Stat | ||
| Number built (qt) |
0
76
43,000
|
|
| Price (USD) |
41.5
35.0 million
750.0 million
|
|
| Introduction | 1997 | |
| First flight | 02.01.1989 | |
