Kamow / Kamov Ka-60 / Ka-62
Medium Utility Helicopter
The Kamov Ka-60 Kasatka and Ka-62 is a twin-engined 16 seat medium utility helicopter developed by the Russian manufacturer Kamov JSC. The Ka-60 is the military variant, the Ka-62 is a civil development.
The prototype is equipped with a four-blade main rotor. The series production helicopters are to be equipped with a five-blade main rotor.
| Propulsion | 2 Turboshaft Engines |
| Engine Model | Saturn RD-600V |
| Engine Power (each) | 959 kW | 1286 shp |
| alternative Engine Variant |
| Engine Model | Turbomeca / HAL Ardiden 1H1 (Shakti) |
| Engine Power (each) | 1032 kW | 1384 shp |
| Speed | 291 km/h | 157 kts
181 mph |
| Service Ceiling | 5.200 m | 17.060 ft |
| Range | 700 km | 378 NM
435 mi. |
| max. Takeoff Weight | 6.500 kg | 14.330 lbs |
| Rotor Blades (main/tail) | 4 / Fenestron |
| Main Rotor Diameter | 13,50 m | 44 ft 3 in |
| Tail Rotor Diameter | 1,20 m | 3 ft 11 in |
| Rotor Disc Area | 143,1 m² | 1540 ft² |
| Length (Fuselage) | 13,46 m | 44 ft 2 in |
| Length | 15,60 m | 51 ft 2 in |
| Height | 4,20 m | 13 ft 9 in |
| First Flight | 24.12.1998 |
| Production Status | in production |
| ICAO Code | KA62 |
| Data for (Version) | Kamow / Kamov Ka-60 (Prototype) |
| Variants | Ka-60 (mil.), Ka-62 (civil) |
