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Initial Operational Capability (IOC):
Total Production: ?
Also Known As: Moskvichka
Origin: Russia
Corporations: Kamov
Parent System: Ka-115
Initial Operational Capability (IOC):
Total Production: ?
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Description: The Ka-115 is a single-engine, light utility helicopter developed by Kamov to carry out transport of cargoes and passengers, patrol, search and rescue, charter flights, medical evacuation, etc. The helicopter's cabin provides seating capacity for up to five passengers plus the pilot. The Ka-115 has two side doors and a rear hatch for quick load/off-load of passengers and cargo and is capable of carrying slung cargoes.

The Ka-115 propulsion system is based on two three-bladed coaxial rotors driven by a single Pratt & Whitney Canada PW206D turboshaft allowing for cruising speeds of 230 kph over ranges in excess of 700 kilometers. Overall, the Ka-115 helicopter provides comfortable and safe flight experience.

Ka-115 Specifications

Crew: 1
Main Rotor Blades: 6
Number of Engines: 1
Passengers: 5
Ceiling: 5,200 meter (17,060 foot)
Hovering Ceiling: 2,350 meter (7,710 foot)
Max Range: 780 kilometer (421 nautical mile)
Climb Rate: 11.5 mps (2,255 fpm)
Cruise Speed: 230 kph (124 KTAS)
Top Speed at High Altitude: 250 kph (135 KTAS)
Max Takeoff Weight: 1,970 kilogram (4,343 pound)
Payload: 700 kilogram (1,543 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

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Propulsion Systems
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