| 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 | |
