In numbers Through the lens Video
Izdeliye 02F
Single-seat, twin-engine, reconnaissance-bomber, which was developed on the basis of the MiG-25RBK, in 1980, while additionally the radio-electronic equipment has been upgraded and has equipped with a new Shar-25 reconnaissance station instead of the Kub-3M.
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia |
| TYPE |
Reconnaissance-bomber
|
| CREW | 1 |
| POWER-PLANT | Two turbojet engines MNPK Soyuz (Khachatourov), R-15B-300 |
| Thrust, kgf | |
| - with afterburning | 2x11.196 |
| - without afterburner | 2x7.495 |
| DIMENSIONS | |
| Length, m | 21,55 |
| 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 | 35.670 |
| Empty aircraft, kg | 19.070 |
| Internal fuel, kg | 14.980 |
| Warload, kg | 5.000 |
| PERFORMANCE | |
| Maximum speed (at high altitude, M=2.83), km/h | 3.000 |
| Maximum speed in low height, km/h | 1.200 |
| Ferry range, km | 2.400 |
| Range, km | 1.865 |
| Rate of climb, m/min | 2.880 |
| Service ceiling, m | 23.000 |
| Maximum overload, g | 5 |
| ARMAMENT | Number external hardpoints: 4. Transportation of weapons: up to 10 bombs, FAB-500. |