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 |