Kamow / Kamov Ka-25
Naval Utility Helicopter
The Kamov Ka-25 is a twin-engined naval ship-based medium utility helicopter with coaxial rotors developed by the Soviet Design Bureau OKB Kamov (OKB-2), today Kamov JSC, Russia. The main roles of the Ka-25 were anti-submarine warfare, electronic warfare, search- and rescue and troop transport (max. 12 soldiers).
Propulsion | 2 Turboshaft Engines |
Engine Model | Glushenkov GTD-3F |
Engine Power (each) | 660 kW | 885 shp |
Speed | 220 km/h | 119 kts 137 mph |
Service Ceiling | 3.353 m | 11.000 ft |
Range | 400 km | 216 NM 249 mi. |
Empty Weight | 4.765 kg | 10.505 lbs |
max. Takeoff Weight | 12.000 kg | 26.455 lbs |
Rotor Blades (main/tail) | 3/3 |
Main Rotor Diameter | 15,74 m | 51 ft 8 in |
Rotor Disc Area | 194,6 m² | 2095 ft² |
Length (Fuselage) | 9,75 m | 31 ft 12 in |
Length | 11,00 m | 36 ft 1 in |
Height | 5,37 m | 17 ft 7 in |
First Flight | 1961 |
Production Status | out of production |
Total Production | ca. 140 |
ICAO Code | KA25 |
NATO Code | Hormone |
Data for (Version) | Kamov / Kamow Ka-25 |
Variants | Ka-25BSh, Ka-25T, Ka-25PS |