Powerplant |
2 x Tumanskiy R13-300 |
Take-off rating |
|
|
dry |
2 x 40,2 kN |
|
reheat |
2 x 64,7 kN |
Length (less pitot) |
20,54 m |
Wing span |
9,34 m |
Wing area |
36,6 m² |
Aileron area |
1,51 m² |
Horizontal tail area |
5,58 m² |
Vertical tail area |
6,951 m² |
|
|
Take-off weight |
|
|
normal (with two R-98 missiles) |
17194 kg |
|
maximum (with two R-98 & R-60 missiles + two drop tanks) |
17900 kg |
Empty weight |
10874 kg |
Landing weight |
12060 kg |
Fuel load (without drop tanks) |
5550 kg |
Thrust/weight ratio |
0,92 |
Wing loading |
397 kg/m² |
Top speed |
|
|
at sea level |
1300 km/h |
|
at high altitude (15000 m) |
2230 km/h |
Mach number at high altitude |
2,16 |
Service ceiling |
18500 m |
G limit |
6,5 |
Unstick speed |
370 km/h |
Landing speed |
285-295 km/h |
Range |
|
|
on internal fuel |
1380 km |
|
with drop tanks |
1700 km |
Endurance |
1 h 41 min |
Interception range |
|
|
head-on mode |
|
| cruise mode |
504 km |
| full military power |
360 km |
| full afterburner |
300 km |
|
pursuit mode |
|
|
cruise mode |
450 km |
|
full military power |
240 km |
|
full afterburner |
55 km |
Take-off run |
1000 - 1100 m |
Landing run |
|
|
without brake chute |
1050 - 1150 m |
|
with brake chute |
850 - 950 |
|
|
Radar type |
Taifoon-M |
Target detection range |
|
|
at high altitude |
65 km |
|
at low altitude |
15 km |
Target trackning range |
|
|
at high altitude |
45 km |
|
at low altitude |
10 km |
Scan limits |
|
|
azimuth |
± 70° |
|
elevation |
+ 30° / - 10° |
|
|
Weapon information |
|
|
R-98M |
|
|
launch range |
|
|
head-on mode (target elevation 4000 - 5000 m) |
5-24 km |
|
pursuit mode |
2-15 km |
|
at low alitude |
2 - 3,5 km |
|
design g-load |
14 g |
|
operational on-wing g-load |
3 g |
|
R-60 |
|
|
launch range |
|
|
head-on mode (target elevation 2000 m) |
- |
|
pursuit mode |
0,2 - 1,6 km |
|
at low alitude |
0,3 - 1,5 km |
|
design g-load |
42 g |
|
operational on-wing g-load |
5 g |
| |
|
