Yak-130
|
DIMENSIONS |
|
|---|---|
| wing span, m | 9.726 |
| overall length, m | 11.493 |
| overall height, m | 4.78 |
| wing area, sq. m | 23.50 |
| sweepback (angle) at 1/4 of chord, degrees | 31 |
|
WEIGHTS |
|
| max takeoff weight, t | 9 000 |
| normal takeoff weight, t | 7 230 |
| max fuel internal tanks capacity, kg | 1 750 |
| max weight of armament, kg | 3 000 |
|
ENGINE |
|
| type, model | Bypass Turbofan Engine, AI-222-25 |
| quantity | 2 |
| max take-off thrust (International Standard Atmosphere,H=0), kg | 2 x 2500 |
| cruising thrust, kg | 2 x 300 |
| thrust/weight/ratio | 0.9 |
|
PERFORMANCE CHARACTERISTICS (ISA) |
|
| max cruising speed, km/h | 1060 |
| max takeoff speed (with max fuel), km/h | 200 |
| max landing speed, km/h | 195 |
| flight range with max fuel, km | 2300 |
| max flight altitude, m | 12 500 |
| max flight time, h | 3 |
| flight attack angles, degrees | 42 |
| take off run (with normal take-off weight), m | 380 |
| landing roll (with normal landing weight), m | 670 |
| flight maneuvering load acceleration | + 8g/ - 3g |
| maximum sustained g-load (H=4 570m (15,000 ft), g | 5.2g |
|
CREW |
|
| flight crew | 2 |
|
SERVICE LIFE |
|
| flight hours | 10 000 |
Description |
Russian |
Western |
Guided "air-to-air" missile |
R-73, R-60 |
AIM-9, Magic |
Guided "air-to-surface" missile |
Kh-25ML / H-25 |
AGM-65 |
Pods with dart 57 mm missiles |
UB-32 |
AL-25-50, LAU-51 |
Bombs of 250-500 kg caliber |
FAB |
Mk82, Mk83, SAMP-25 |
Cluster munition |
RBK-500 |
BL 755 |
Laser-guided bombs |
ÊÀB-500 |
Rockeye II |
incendiary tanks |
ZB-500 |
|
unguided missiles |
S-8 |
|
Gun pod |
23 mm GSh-23L |
DEFA, Aden |
Drop fuel tanks |
|
|
Pod with laser-TV guidance system |
|
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