In numbers Through the lens Video
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY |
Russia
|
| TYPE |
Reconnaissance aircraft
|
| CREW | 1 |
| POWER-PLANT | Two turbojet 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 |
| Maximum speed on a reconnaissance mission, km/h | 2.650 |
| Maximum speed in low height, km/h | - |
| Range, km | |
| - at supersonic speed without external fuel tanks | 1.635 |
| - at subsonic speed without external fuel tanks | 1.865 |
| - at supersonic speed with external fuel tanks | 2.130 |
| - with speed Μ=2,35 | 1.250 |
| - with two external fuel tanks (5.300 l) with subsonic speed | 2.400 |
| Rate of climb, m/min | 18.000 |
| Service ceiling, m | 23.000 |
| Maximum overload, g | 5 |
| EQUIPMENT | 3-5 (2 to 4 AFA A-70M or one topographic type AFA-E/10). Hight resolution cameras with a lateral rotational system. |
| ARMAMENT | Doesn't have (defensive). |