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 |