| Type | Aircraft | |
| Company | Joint Stock Company Tupolev | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
53.1
88.7
|
|
| Height (m) |
0.6
14.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
311.1
925
|
|
| Wingspan (Beam) (m) |
0.1
50
95
|
|
| Weights | ||
| Empty weight (kg) |
8
93,000
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
185,000
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
10
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
925
28,165
|
|
| Сruise Speed (km/h) |
52
711
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
108,750
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
60,000
60,000
|
4 powerplants 15000 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
13,500
161,544
|
|
| Range (Ferry range) (km) |
4
12,550
40,700
|
|
| Сombat radius (km) |
277
6,400
7,210
|
|
| Takeoff roll (m) |
20
3,200
3,200
|
|
| Stat | ||
| Number built (qt) |
0
100
43,000
|
|
| Introduction | 1968 | |
| First flight | 18.07.1968 | |
