Ka-62

Medium Class Helicopter

Multifunctionality

Flight safety

Payload

2500 kg/ 15 pax

Flight range

760 km

Cruise speed

290 km/h

Description

The new medium multirole Ka-62 helicopter incorporates the latest technologies and materials in aircraft building. It meets Russian and international flight standards (Russia’s AP-29, Europe’s CS-29 and JAR-OPS3), offshore operational requirements, international standards for reliability, resource use, flight safety, comfort, usability, service life and repair.

  • The Ka-62 is fitted with two Ardiden 3G 1,776 h.p. engines made by SAFRAN HE. Their modular design and dual-channel FADEC system ensures high reliability, heightened ease of operation, and low fuel use. The helicopter is also equipped with a glass cockpit developed by the Russian company Transas.
  • The Ka-62 is built to a single-rotor design with a multi-blade anti-torque rotor ducted into the vertical tail fin. It has a five-bladed main rotor, enclosed tail rotor, secondary hydraulics circuit, heavy-duty wheeled landing gear, strengthened fuselage and mounting attachments for major components, as well as shock-absorbent seats for passengers and crew.
  • The airframe and propeller blades will be over 50% made of polymeric composite materials.

The Ka-62 is designed for cargo transportation, medevac and search and rescue operations, and can also be used in the oil and gas sector and for corporate purposes.

The Ka-62 has the following competitive advantages:

  • It can operate in a wide range of climate and geographic conditions;
  • It can operate in external air temperatures from –50°С до +50°С;
  • It operates in temperatures down to –35°С without any need to heat the transmission assemblies and engines;
  • The Ka-62 can fly in adverse weather conditions, and into known icing conditions;
  • The Ka-62 can be operated from an airbase, oil platform and unprepared ground areas;
  • The Ka-62 is capable of autonomous deployment and does not need to be stored in a hangar. 

Characteristics

Performance

Max. speed

310 km/h

Cruise speed

290 km/h

Rate of climb

14 m/s

Hover ceiling (OGE

3200 м

Operational ceiling

6100 м

Max. flight range with main fuel tanks

760 км

Max. flight range with additional fuel tanks

1135 км

Duration of flight with standard fuel

4 h

Weight Parameters

Max. take-off weight

6800 kg

Max. payload on external sling

2500 kg

Max. payload in transport cabin

2000 kg

Engines

Turboshaft engines

2xArdiden3G

Take-off power

2 x 1776 h.p.

Max. continuous power

2 x 1546 h.p.

Contingency power

1 x 1940 h.p.

Dimensions

Length

13470 mm

Fuselage Width

1895 mm

Height

4865 mm

Rotor diameter

13800 mm

Length of cabin

4100 mm

Width of cabin

1740 mm

Height of cabin

1300 mm

Capacity

Air crew

1-2 pax

Passengers

up to 15 pax
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