In numbers Through the lens Video
Three-view drawing
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 | 1x13.100 |
| Thrust-to-weight ratio | 0,88 |
| DIMENSIONS | |
| Length, m | 16,10 |
| Length + pitot, m | 18,10 |
| Height, m | 4,50 |
| Wing span, m | |
| - minimal | 7,80 |
| - maximum | 14,00 |
| Wing area, m2 | 32,4 / 35,5 / 37,7 |
| - minimal | 32,4 |
| - average | 35,5 |
| - maximum | 37,7 |
| Horizontal stabilizer span, m | 5,25 |
| LANDING GEAR | Retractable landing gears with a double nose wheel and a single-wheel system on the main gears. |
| Wheel base, m | 5,77 |
| Wheel track, m | 2,66 |
| WEIGHT | |
| Maximum take-off, kg | 17.800 |
| Normal take-off, kg | 14.800 |
| Empty aircraft, kg | 10.000 |
| Internal fuel, kg | 5.750 |
| Fuel capacity in external tanks, kg | 3x800 |
| Warload, kg | 1.300 |
| - normal | 3.300 |
| - maximum | 4.500 |
| Wing loading, kg/m2 | 417 |
| PERFORMANCE | |
| Maximum Mach number | 2,35 |
| Maximum speed, km/h | 2.500 |
| Cruising speed, km/h | 800 |
| Maximum speed in low height, km/h | 1.400 |
| Rate of climb, m/s | 240 |
| Service ceiling, m | 18.300 |
| Combat range, km | 960 |
| Range, km | 2.500 |
| Take-off distance, m | 500 |
| Landing distance, m | 750 |
| Maximum overload, g | 8,5 |
| EQUIPMENT |
Radar S-23MLD SAPFIR. Detection range 85 km. Range for target jamming 60 km. Number of detected and tracked targets 4. Number of simultaneous attacks against targets 2. Antenna diameter 0,9 m.
|
| ARMAMENT | One 23-mm GSh-23L with 200 rounds. Number external hardpoints: 6. Transportation of weapons: 2xR-23, R-24, 4xR-60, air-to-surface Kh-23, Kh-25, Kh-29, UR S-5, S-8, S-13 and S-24 pods with cannons, bombs KAB-500KR/L, AB-500. External fuel tank type PTB-800, nuclear bomb. |
Photos MiG-23 Flogger, Air Force Museum (VVS), Monino, Russia.
MiG-23 Flogger, Museum of History of Ukraine in World War II, Kyiv.
