Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
38.6
88.7
|
|
Height (m) |
0.6
11.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
174.5
925
|
|
Wingspan (Beam) (m) |
0.1
34.5
95
|
|
Weights | ||
Empty weight (kg) |
8
43,000
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
76,000
575,000
|
|
Capacity | ||
Crew (per.) |
1
6
112
|
|
Useful load (kg) |
26.4
10,000
90,700
|
|
Payload (kg) |
23
10,000
122,470
|
|
Capacity passengers (per.) |
1
70
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
950
28,165
|
|
Сruise Speed (km/h) |
52
775
3,087
|
|
Power | ||
Thrust (kN) |
1.5
186.4
1,914
|
2 powerplants 93,2 kW each |
Performance | ||
Service ceiling (m) |
0.6
11,750
161,544
|
|
Range (Ferry range) (km) |
4
3,300
40,700
|
with 10,000 kg payload, 775 km/h at 10,000 m |
Takeoff roll (m) |
20
1,970
3,200
|
|
Landing roll (m) |
20
1,850
2,570
|
|
Combat | ||
Guns (qt) |
1
2
18
|
23mm Afanasev Makarov AM-23 cannon |
Stat | ||
Number built (qt) |
0
1
43,000
|
|
Introduction | 1958 | |
First flight | 1958 |