| Type | Aircraft | |
| Company | SC A.S. Yakovlev Design Bureau | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
21.6
88.7
|
|
| Height (m) |
0.6
4.0
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
37.6
925
|
|
| Wingspan (Beam) (m) |
0.1
12.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
9,970
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
20,000
575,000
|
|
| Loaded weight (kg) |
5
15,000
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
1,840
28,165
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
4,615
320,000
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.6
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
124
980
|
2 powerplants 62 kN each |
| Thrust (kN) |
1.5
92
1,914
|
2 powerplants 46 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
16,750
161,544
|
|
| Range (Ferry range) (km) |
4
2,500
40,700
|
|
| Endurance (h) |
0.0
2.3
150
|
|
| Combat | ||
| Missiles (qt) |
1
4
24
|
2 × R-98M (AA-3 'Anab') air-to-air missiles, usually one R-98TM infrared and one R-98RM semi-active radar homing; 2 × K-13A (AA-2 'Atoll') short-range missiles (occasionally fitted) |
| Stat | ||
| Number built (qt) |
0
1,180
43,000
|
|
| Introduction | 1962 | |
| First flight | 05.03.1958 | |
| Stop production | 1992 | |
