Mikojan Gurewitsch / Mikoyan Gurevich MiG-25
Fighter
The Mikoyan-Gurevich MiG-25 is a twin-engine single-seat jet fighter for the interceptor-role and aircraft developed by the Soviet Design Bureau Mikoyan-Gurevich OKB.
| Crew | 1 | |
| Propulsion | 2 Turbojet Engines | |
| Engine Model | Tumansky R-15B-300 | |
| Engine Power (each) dry/with Afterburner | 73,5 / 100,1 kN | 16524 / 22494 lbf |
| Speed | 3000 km/h | 1620 kts 1864 mph |
| Service Ceiling | 21.000 m | 68.897 ft |
| Range | 2.130 km | 1.150 NM 1.323 mi. |
| Empty Weight | 19.070 kg | 42.042 lbs |
| max. Takeoff Weight | 41.200 kg | 90.830 lbs |
| Wing Span | 13,42 m | 44 ft 0 in |
| Wing Area | 56,8 m² | 611 ft² |
| Length | 21,55 m | 70 ft 8 in |
| Height | 6,50 m | 21 ft 4 in |
| First Flight | 1964 | |
| Production Status | out of production | |
| Total Production | 1190 | |
| ICAO Code | MG25 | |
| NATO Code | Foxbat | |
| Data for (Version) | Mikoyan-Gurevich / Mikojan-Gurewitsch MiG-25RB | |
| [Photo-ID: 13065] © Arjun Sarup 2007-01-08 | |
 | Mikojan Gurewitsch / Mikoyan Gurevich MiG-25 Indian Air Force Reg.: KP355 c/n: 20563 On display at IAF Museum Palam. |
| [Indira Gandhi International Airport (VIDP / DEL)] | |