In numbers Through the lens Video
NATO reporting name: Foxbat F
izdeliye 02M
izdeliye 66
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia |
| TYPE |
Fighter
|
| CREW | 1 |
| POWER-PLANT | Two turbojet engines R-15BD-300 |
| Thrust, kgf | |
| - with afterburning | 2x11.196 |
| - without afterburner | 2x8.800 |
| DIMENSIONS | |
| Length, m | 22,27 |
| Height, m | 6,00 |
| Wing span, m | 13,42 |
| Wing area, m2 | 61,40 |
| WEIGHT | |
| Maximum take-off, kg | 41.200 |
| Normal take-off, kg | 37.000 |
| Empty aircraft, kg | 20.600 |
| Internal fuel, kg | - |
| Warload, kg | up to 5.000 |
| PERFORMANCE | |
| Maximum speed (at high altitude, M=2.83), km/h | 3.000 |
| Cruising speed, km/h | 2.345 |
| Maximum speed in low height, km/h | 1.200 |
| Range, km | 3.200 |
| Combat range, km: | |
| - supersonic speed | 1.635 |
| - subsonic speed | 1.865 |
| - supersonic speed + external fuel tank (5.300 l) | 2.130 |
| - external fuel tank (5.300 l) with subsonic speed | 2.400 |
| Rate of climb, m/min | 2.900 |
| Service ceiling, m | 23.000 |
| Maximum overload, g | 5 |
| ARMAMENT | Ability to transport up to 2-4xR-60M, Kh-58U or weapons load up to 5.000 kg (when it comes to bombs of various calibers). |