In numbers Through the lens Video
Also identified as: MiG-23B-98, MiG-23UB-99
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia |
| TYPE |
Multipurpose Fighter
|
| CREW | 1 |
| POWER-PLANT | One turbojet engine MNPK Soyuz (Khachatourov), R-35-300 |
| Thrust, kgf | 1x13.000 |
| DIMENSIONS | |
| Μήκος, m | 16,70 |
| Length, m | 4,35 |
| Wing span, m | |
| - minimal | 7,80 |
| - maximum | 14,00 |
| Wing area, m2 | |
| - minimal | 23,35 |
| - maximum | 35,50 |
| WEIGHT | |
| Maximum take-off, kg | 18.400 |
| Normal take-off, kg | 14.700 |
| Empty aircraft, kg | 10.900 |
| Internal fuel, kg | - |
| Warload, kg | 2.500 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.450 |
| Cruising speed, km/h | 990 |
| Service ceiling, m | 19.000 |
| Combat range, km | 1.470 |
| Range, km | 2.360 |
| ARMAMENT | 1x23 mm cannon GSh-23L. Number external hardpoints: 5. Transportation of weapons: - 4xR-77 or R-73 - 6xR-60 - 2xR-23, R-24 - 2xKh-31 or Kh-35 or Kh-29T - 4xKAB-500 or bombs 500 kg, FAB-500. |