In numbers Through the lens Video
Izdeliye 02V
The MiG-25RBV was developed based on the MiG-25RB. The aircraft was identical to the "RB" variant with the only difference being that instead of the SPS-4A/B station, the "SPS-9 or known as Virazh-1" electronic reconnaissance equipment was installed. To distinguish the version, all aircraft equipped with the “SPS-9” type station they were renamed MiG-25RBV.
The MiG-25RBV was mass produced in 1973-1979.
Technical specifications
| 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 | 6,50 |
| 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. |