In numbers Through the lens Video
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia |
| TYPE |
Flying laboratory
|
| CREW | 1 |
| POWER-PLANT | Two tuebojet engines MNPK Soyuz (Khachatourov), R-15B-300 |
| Thrust, kgf | 2x11.196 |
| DIMENSIONS | |
| Length, m | 22,30 |
| Height, m | 6,50 |
| Wing span, m | 14,06 |
| Wing area, m2 | 61,90 |
| WEIGHT | |
| Maximum take-off, kg | 41.000 |
| Normal take-off, kg | 34.720 |
| Empty aircraft, kg | 18.800 |
| Internal fuel, kg | 14.470 |
| Warload, kg | - |
| PERFORMANCE | |
| Maximum speed (at high altitude, M=2.83), km/h | 3.000 |
| Cruising speed, km/h | - |
| Maximum speed in low height, km/h | 1.200 |
| Range, km | |
| - at speed M=2,35 | 1.250 |
| - at subsonic speed | 1.730 |
| Service ceiling, m (+ 4 missiles), m | 20.700 |
| Maximum overload, g | 5 |
| ARMAMENT | It doesn't have a gun. Number external hardpoints: 4. Transportation of weapons: to 4xR-40T or R-40R. |