In numbers Through the lens Video
NATO reporting name: Foxbat C
izdeliye 39
Also recognized as: MiG-25PU-SOTN, MiG-25RBK
The only aircraft was reequipped to test systems and ejection seats K-36RB, designed for the Buran spacecraft.
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia |
| TYPE |
Trainer aircraft
|
| CREW | 1 |
| POWER-PLANT | Two turbojet engines MNPK Soyuz (Khachatourov) R-15B-300 |
| Thrust, kgf | 2x11.200 |
| DIMENSIONS | |
| Length, m | 21,55 |
| Height, m | 6,50 |
| Wing span, m | 13,42 |
| Wing area, m2 | 61,40 |
| WEIGHT | |
| Maximum take-off, kg | 36.720 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 18.760 |
| Internal fuel, kg | - |
| Warload, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 2.800 |
| Maximum speed in low height, km/h | 1.200 |
| Ferry range, km | 2.400 |
| Range, km | 1.200 |
| Rate of climb, m/min | 2.880 |
| Service ceiling, m | 20.000 |
| Maximum overload, g | 4,5 |
| ARMAMENT | Doesn't have (defensive). |