In numbers Through the lens Video
Three-view drawing
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia, Israel |
| TYPE |
Front-line attack fighter
|
| CREW | 1 |
| POWER-PLANT | One turbojet engine R-25-300 |
| Thrust, kgf | 1x7.100 |
| DIMENSIONS | |
| Length, m | 15,76 |
| Height, m | 4,71 |
| Wing span, m | 7,154 |
| Wing area, m2 | 23,00 |
| WEIGHT | |
| Maximum take-off, kg | 10.500 |
| Normal take-off, kg | 8.825 |
| Empty aircraft, kg | 5.350 |
| Internal fuel, kg | - |
| Warload, kg | 1.500 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.230 |
| Maximum permitted speed at high altitude, km/h | - |
| Maximum speed in low height, km/h | 1.300 |
| Range with external fuel tanks, km | 2.100 |
| Range, km | 1.800 |
| Combat range, km | 350-750 |
| Rate of climb, m/min | 15.250 |
| Service ceiling, m | 18.500 |
| Maximum overload, g | 8,5 |
| ARMAMENT | 2x23 mm cannon GSh-23L. Number external hardpoints: 5. Transportation of weapons: Python-4 missile or similar missiles of the third and fourth generation. Air guided and unguided rockets. |