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 |