Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
22.0
88.7
|
|
Height (m) |
0.6
5.7
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
67.4
925
|
|
Wingspan (Beam) (m) |
0.1
21.7
95
|
|
Weights | ||
Empty weight (kg) |
8
14,930
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
25,350
575,000
|
|
Loaded weight (kg) |
5
20,930
242,500
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Speeds | ||
Ground Speed (km/h) |
96.6
800
1,500
|
|
Max. Speed (km/h) |
25
848
28,165
|
|
Fuel | ||
Fuel Capacity (l) |
23
4,365
320,000
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.3
2.1
|
|
Thrust (kN) |
1.5
53
1,914
|
2 powerplants 26,5 kN each |
Performance | ||
Service ceiling (m) |
0.6
11,300
161,544
|
|
Range (Ferry range) (km) |
4
2,930
40,700
|
|
Сombat radius (km) |
277
1,200
7,210
|
|
Combat | ||
Guns (qt) |
1
4
18
|
2 × 23 mm NR-23 cannon forward; 2 × 23 mm NR-23 cannon in tail turret |
Bombs weight (kg) |
2
3,000
39,000
|
bombs, mines or torpedoes |
Stat | ||
Number built (qt) |
0
150
43,000
|
|
Introduction | 1952 | |
First flight | 13.10.1949 | |
Stop production | 1959 |