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Revision as of 08:28, 10 February 2012
| Ka-226 | |
|---|---|
| |
| Ka-226T at MAKS 2005 | |
| Role | Light utility |
| National origin | Russia |
| Manufacturer | Kamov |
| First flight | 4 September 1997 |
| Introduction | 2002 |
| Developed from | Kamov Ka-26 |
The Kamov Ka-226 "Sergei" is a small, twin-engined Russian utility helicopter. The Ka-226 features an interchangeable mission pod, rather than a conventional cabin, allowing the use of various accommodation or equipment configurations. The Ka-226 entered service in 2002.
Variants of the Ka-226 have the NATO reporting name of Hoodlum, however Kamov's own name for the Ka-226 is Sergei.
Development
A twin turbine version of the successful Kamov Ka-26, (a single turbine version was called the Kamov Ka-126) the Ka-226 was initially announced in 1990. Originally developed to meet the requirements of the Russian disaster relief ministry, the aircraft first flew on 4 September 1997. Certification to Russian AP-29 'A' and 'B' transport categories was granted on 31 October 2003. The Ka-226 entered production at "Motor Sich", Zaporozhye, Ukraine.
Design
The design is a refinement of the proven Ka-26, featuring interchangeable mission pods. The aircraft is fitted with a new rotor system, increased visibility nose, and new passenger cabin design. The Ka-226 also features a new transmission system and is made largely from composite materials.
The aircraft is fitted with trademark Kamov coaxial rotors, of advanced composite design, making the Ka-226 highly maneouverable and eliminating the need for a tail rotor.
Variants
Search and rescue, medivac, disaster relief and patrol variants have been developed for the Russian Emergency Ministry. Air ambulance, police and fire fighting variants have been developed for the Russian government.
- Ka-226A : Utility helicopter.
- Ka-226-50 : Described initially as "improved version", but now appears to apply to all standard models.
- Ka-226AG : Gazprom specific variant.
- Ka-226T : Instead of Rolls-Royce 250C engines, this variant is fitted with the more powerful Turbomeca Arrius 2G2. Each engine provides 670 shp, increasing the service ceiling to around 7000m, providing improved high altitude and high temperature operation.[1]
- Ka-226U : Dual control training variant.
Operators
- The Russian federal security service, which is in charge of border protection, took delivery of two Ka-226 helicopters and is considering buying another version equipped with more powerful Turbomeca Arrius 2G2 turboshaft engines (Ka-226T).[2]
- Two Ka-226 helicopters have been delivered to the Moscow police service.[2]
- Russian gas company Gazprom operate several Ka-226 helicopters, designated Ka-226AG (AG standing for Gazprom company). The only difference from the standard Ka-226 is a different avionics fit.[3]An initial batch of 14 aircraft was due to be delivered during 2007.[2]
- Six Ka-226 helicopters with Rolls-Roye engines have been ordered by the Russian MOD in 2011.[4]
- A $25 million contract has been signed with Jordan to provide the RJAF with 6 Ka-226 helicopters. They will be partially assembled in Jordan at the Russian-Jordanian Oboronprom Middle East helicopter assembly facility. The deal is a breakthrough for Russian helicopter manufacturers as Jordan previously bought only Western-built rotorcraft.[5]
Specifications (Ka-226A)
Data from www.kamov.ru
General characteristics
- Crew: 1
- Passengers: 9
- Cargo: 1,400kg internally, or 1,500kg on an external sling
Performance
See also
Related development
Aircraft of comparable role, configuration, and era
References
- ^ "The Ka-226 helicopter with new engines powered is under testing". Kamov Company. Archived from the original on 2008-02-29. Retrieved 2008-06-04.
- ^ a b c "Turnaround Nears for Russia's Helicopter Sector". Aviation Week. February 2007. Retrieved 2008-06-04.
- ^ "Gas giant gets first of big Kamov helicopter order this summer". newsnations.com. July 2004. Retrieved 2008-06-04.
- ^ http://www.russiandefenseblog.org/?p=1793
- ^ "Putin visit ignites demand for Russian helos in Mideast". AINonline. November 2007. Retrieved 2008-06-04.
The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.
External links
