Ka-62

Description

General Information

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 1,680 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 +45°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. 

Features
Performance
Max. speed
308 km/h
Cruise speed
290 km/h
Max. flight range with main fuel tanks
770 km
Operational ceiling
5,700 m
Hover ceiling (OGE)
3,300 m

Weight Parameters

Max. take-off weight
6,500 kg

Max. Payload, kg

in transport cabin
2,000
on external sling
2,500

Engines 2хArdiden 3G, Turbomeca

Take-off power
1,776 h.p.
Contingency power
1,941 h.p.

Dimensions of Сargo Сabin

Length
4,100 mm
Maximum floor width
1,750 mm
Height
1,300 mm
Volume
9.5 m3

Capacity:

Air crew
1–2 persons
Service passengers
12–15 persons
Photos
© 2018 ‘Russian Нelicopters, JSC’
115054, Bolshaya Pionerskaya, 1, Moscow, Russia