Kamow Ka-226

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Kamov Ka-226 Sergei
Kamow Ka-226T at MAKS, 2005
Kamow Ka-226T at MAKS, 2005
Type: Light multipurpose helicopter
Design country:

RussiaRussia Russia

Manufacturer:

Kamov

First flight:

4th September 1997

Commissioning:

2002

Production time:

since 2002

Number of pieces:

269 ​​orders (as of 2017)

The Kamow Ka-226 Sergei ( Russian Камов Ка-226 Сергей ) is a light multi-purpose helicopter that has been manufactured in Russia by the Kamow company since 1997 .

history

The Ka-226, announced in 1990, was designed to replace the aging fleet of the previous version Kamow Ka-26 , which is still powered by piston engines. By contrast, the new type has two Allison 250 - turbines . The need for such universal helicopters is high in Russia, for example for the maintenance of the energy supply infrastructure, for disaster control , air surveillance or the supply of remote settlements in Siberia.

The helicopter had its maiden flight on September 4, 1997 and received its Russian approval on October 31, 2003 . The Ka-226T version with the more powerful Turbomeca Arrius 2G1 has been in testing since 2009 . Series production started in 2011.

In February 2017 it was announced that 200 Ka-226Ts will be delivered to the Indian Armed Forces starting in 2019. 60 of these are to be delivered from Russia. 140 pieces are to be built in India.

construction

Like its predecessor models, the helicopter has the typical Kamow coaxial rotor . From the 26 model he also inherited the principle of modular construction, in which the passenger cabin behind the cockpit can be expanded as a whole. Instead, module containers with medical equipment or containers for agricultural chemicals with a spray device for agricultural use can be installed. Without any module, instead equipped with a winch , the Ka-226 is also used for transporting external loads.

Technical specifications

Parameter Data Ka-226 Data Ka-226T
constructor Leonid Shiryaev
crew 1-2
Passengers Max. 8th 7th
Rotor diameter 13.00 m
length 8.10 m
height 4.25 m with rotor head
Empty mass 1952 kg
Max. Takeoff mass 3400 kg 3600 kg
Top speed 210 km / h 250 km / h
Cruising speed 185 km / h
Service ceiling 3500 m 6100 m
Rate of climb 10.1 m / s
Range 600 km
Engines two Rolls-Royce Allison 250 -C20B two Turbomeca Arrius 2G1
power 313 kW each (420 WPS) 500 kW each (670 WPS)

Users

Ka-226AG from Gazpromavia at MAKS 2007
RussiaRussia Russia
IndiaIndia India

Web links

Commons : Kamow Ka-226  - Album with pictures, videos and audio files

Individual evidence

  1. Turbomeca website about the Arrius 2G1 for the Kamov-226T ( Memento from May 7, 2016 in the Internet Archive )
  2. Russia to start deliveries of helicopters to India in 2019 | Reuters . In: archive.is . February 21, 2017 ( reuters.com [accessed March 29, 2017]).
  3. ^ Claudio Müller: Planes of the World 2012 . 1st edition. Motorbuch Verlag, Stuttgart 2012, ISBN 978-3-613-03421-1 , p. 221 f .
  4. Ka-226T Features. In: russianhelicopters.aero. Retrieved November 1, 2018 .
  5. http://bmpd.livejournal.com/1573843.html
  6. http://bmpd.livejournal.com/1975938.html
  7. a b World Air Forces 2016 . Flightglobal Insight. 2016. Retrieved May 28, 2016.
  8. Alexander Mladenov: Federal Security Ka-226Ts . In: Air International . 89, No. 5, November 2015, ISSN  0306-5634 , p. 35.
  9. Stanley Carvalho: Russia to start deliveries of helicopters to India in 2019 . February 20, 2017. Retrieved February 21, 2017.