Jakowlew / Yakovlev Jak-24 / Yak-24
Transport Helicopter
The Yakovlev Yak-24 is a twin-engined tandem rotor medium transport helicopter developed by the Soviet Design Bureau OKB Yakovlev (OKB-115).
| Propulsion | 2 Radial Engines |
| Engine Model | Shvetsov ASh-82V(W) |
| Engine Power (each) | 1268 kW | 1700 hp |
| Speed | 194 km/h | 105 kts
121 mph |
| Service Ceiling | 4.200 m | 13.780 ft |
| Range | 267 km | 144 NM
166 mi. |
| Empty Weight | 10.607 kg | 23.384 lbs |
| max. Takeoff Weight | 15.830 kg | 34.900 lbs |
| Rotor Blades (main/tail) | 4/4 |
| Main Rotor Diameter | 20,20 m | 66 ft 3 in |
| Tail Rotor Diameter | 20,20 m | 66 ft 3 in |
| Rotor Disc Area | 320,5 m² | 3450 ft² |
| Length | 21,34 m | 70 ft 0 in |
| Height | 6,50 m | 21 ft 4 in |
| First Flight | 03. Jul. 1953 |
| Production Status | out of production |
| Production Range | 1956-1958 |
| Total Production | 40 |
| NATO Code | Horse |
| Data for (Version) | Yakovlev Yak-24 / Jakowlew Jak-24 |
