Kamow / Kamov Ka-32
Medium Utility Helicopter
Photo ©: Mike Vallentin
The Kamov Ka-32 is a twin-engined 18 seat medium civil utility helicopter with coaxial rotors developed by the Soviet Design Bureau OKB Kamov (OKB-2), today Kamov JSC, Russia.
| Propulsion | 2 Turboshaft Engines |
| Engine Model | Klimov TW3-117VMA / TV3-117VMA |
| Engine Power (each) | 1638 kW | 2197 shp |
| Speed | 250 km/h | 135 kts
155 mph |
| Service Ceiling | 6.096 m | 20.000 ft |
| Range | 850 km | 459 NM
528 mi. |
| Empty Weight | 6.500 kg | 14.330 lbs |
| max. Takeoff Weight | 12.600 kg | 27.778 lbs |
| Rotor Blades (main/tail) | 3/3 |
| Main Rotor Diameter | 15,90 m | 52 ft 2 in |
| Rotor Disc Area | 198,6 m² | 2138 ft² |
| Length (Fuselage) | 11,30 m | 37 ft 1 in |
| Length | 12,25 m | 40 ft 2 in |
| Height | 5,40 m | 17 ft 9 in |
| First Flight | 12/1974 |
| Production Status | in production |
| ICAO Code | KA27 |
| NATO Code | Helix |
| Data for (Version) | Kamov / Kamow Ka-32T |
