| Type | Aircraft | |
| Company | Joint Stock Company Tupolev | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
56.5
88.7
|
|
| Height (m) |
0.6
16.1
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
311.1
925
|
|
| Wingspan (Beam) (m) |
0.1
51.4
95
|
|
| Rotors | ||
| Rotor number (qt) |
1
8
8
|
|
| Weights | ||
| Empty weight (kg) |
8
103,000
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
175,000
575,000
|
|
| Loaded weight (kg) |
5
171,000
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
24
112
|
12 + full spare crew |
| Speeds | ||
| Max. Speed (km/h) |
25
790
28,165
|
|
| Сruise Speed (km/h) |
52
520
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
84,327.3
320,000
|
|
| Power | ||
| Power/mass (hp/kg) |
0.0
0.4
22.1
|
|
| Total Power (hp) |
0.4
59,000
60,000
|
4 powerplants 14795 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
10,700
161,544
|
|
| Range (Ferry range) (km) |
4
7,000
40,700
|
with internal fuel only |
| Endurance (h) |
0.0
20
150
|
with 1 in-flight refuel |
| Propellers | ||
| Prop blade number (qt) |
1
8
8
|
|
| Stat | ||
| Number built (qt) |
0
12
43,000
|
|
| Introduction | 1962 | |
| First flight | 23.01.1962 | |
| Stop production | 1984 | |
