Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
42.4
88.7
|
|
Height (m) |
0.6
11.1
50.1
|
|
Wings | ||
Wingspan (Beam) (m) |
0.1
34.3
95
|
20° sweep |
0.1
23.3
95
|
65° sweep | |
Weights | ||
Empty weight (kg) |
8
68,000
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
124,000
575,000
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
pilot, co-pilot, navigator, weapon systems operator |
Hardpoints (qt) |
1
3
2,576
|
Raduga Kh-22 missiles in weapons bay and on wing pylons or |
1
10
2,576
|
6 × Raduga Kh-15 missiles on a MKU-6-1 rotary launcher in its bomb bay, plus 4 × Raduga Kh-15 missiles on two underwing pylons | |
1
69
2,576
|
69 × FAB-250 or 8 × FAB-1500 might be typical | |
Speeds | ||
Ground Speed (km/h) |
96.6
1,050
1,500
|
|
Max. Speed (km/h) |
25
2,300
28,165
|
|
Сruise Speed (km/h) |
52
930
3,087
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.5
2.1
|
|
Thrust (kN) |
1.5
495.8
1,914
|
2 powerplants 247,9 kN each |
Performance | ||
Service ceiling (m) |
0.6
13,300
161,544
|
|
Range (Ferry range) (km) |
4
6,800
40,700
|
|
Takeoff roll (m) |
20
2,000
3,200
|
2000—2100 m |
Landing roll (m) |
20
1,200
2,570
|
1200—1300 m |
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
900
36,000
|
|
Combat | ||
Guns (qt) |
1
1
18
|
23-mm GSh-23 cannon |
Stat | ||
Number built (qt) |
0
497
43,000
|
|
Introduction | 1972 | |
First flight | 30.08.1969 |