In numbers Through the lens Video
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia |
| TYPE |
Experimental plane
|
| CREW | 1 |
| POWER-PLANT | Two turbojet engines R-15BF2-300 |
| Thrust, kgf | 2x13.500 |
| DIMENSIONS | |
| Length, m | 22,30 |
| Height, m | 6,50 |
| Wing span, m | 14,07 |
| Wing area, m2 | 61,90 |
| WEIGHT | |
| Maximum take-off, kg | 41.000 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 18.900 |
| Internal fuel, kg | - |
| Warload, kg | - |
| PERFORMANCE | |
| Maximum speed (at high altitude, M=2.83), km/h | 3.200 |
| Cruising speed, km/h | 2.345 |
| Maximum speed in low height, km/h | 1.250 |
| Ferry range, km | 3.200 |
| Range, km | 1.730 |
| Service ceiling, m | 21.000 |
| ARMAMENT | Number external hardpoints: 4. Transportation of weapons: up to four R-40T or R-40R or R-60. |