Jakowlew / Yakovlev Jak-25 / Yak-25
Interceptor
The Yakovlev Yak-25 is a twin-engined two-seat fighter aircraft for the interceptor role developed by the Soviet Design Bureau OKB Yakovlev (OKB-115). The version Yak-25RV is a single-seat reconaissance variant.
Propulsion | 2 Turbojet Engines |
Engine Model | Mikulin AM-5A |
Engine Power (each) | 19,6 kN | 4406 lbf |
Speed | 1091 km/h | 589 kts 678 mph |
Service Ceiling | 14.500 m | 47.572 ft |
Range | 2.100 km | 1.134 NM 1.305 mi. |
Empty Weight | 5.678 kg | 12.518 lbs |
max. Takeoff Weight | 11.500 kg | 25.353 lbs |
Wing Span | 10,96 m | 35 ft 11 in |
Wing Area | 31,5 m² | 339 ft² |
Length | 15,67 m | 51 ft 5 in |
Height | 4,35 m | 14 ft 3 in |
First Flight | 19. Jun. 1952 |
Production Status | out of production |
Production Range | 1954-1957 |
Total Production | 638 |
NATO Code | Flashlight Mandrake |
Data for (Version) | Yakovlev Yak-25 / Jakowlew Jak-25 |