Mikojan Gurewitsch / Mikoyan Gurevich MiG-31
Interceptor
The Mikoyan-Gurevich MiG-31 is a twin-engine two-seat jet fighter aircraft for the interceptor-role developed by the Soviet Design Bureau Mikoyan-Gurevich OKB.
| Propulsion | 2 Turbofan Engines |
| Engine Model | Soloviev D-30F-6 |
Engine Power (each) dry/with Afterburner | 93,0 / 152,0 kN | 20907 / 34171 lbf |
| Speed | 3000 km/h | 1620 kts 1864 mph |
| Service Ceiling | 20.600 m | 67.585 ft |
| Range | 720 km | 389 NM 448 mi. |
| Empty Weight | 21.825 kg | 48.116 lbs |
| max. Takeoff Weight | 46.200 kg | 101.853 lbs |
| Wing Span | 13,40 m | 43 ft 12 in |
| Wing Area | 61,6 m² | 663 ft² |
| Length | 22,60 m | 74 ft 2 in |
| Height | 6,10 m | 20 ft 0 in |
| First Flight | 17.09.1975 |
| Production Status | out of production |
| Total Production | ca. 220 |
| ICAO Code | MG31 |
| NATO Code | Foxhound |
| Data for (Version) | Mikoyan-Gurevich / Mikojan-Gurewitsch MiG-31 |