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Izdeliye 02K
Izdeliye 52
A single-seat, twin-engine supersonic reconnaissance bomber was created on the basis of the MiG-25RB aircraft in 1972.
MiG-25RBK was distinguished by the presence of a complex of detailed electronic intelligence "Kub-3M". There was no aerial camera equipment on the plane and it was not installed, transparent hatches for aerial cameras were covered with metal.
Serial production of the MiG-25RBK was carried out from 1973 to 1980.
MiG-25RBK reconnaissance-bomber export version with simplified guidance and weapon control equipment was supplied to Algeria, Iraq, Libya, Syria, India and Bulgaria.
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. |