Kamov Ka-60

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Ka-60 Kasatka
300px
Ka-62 serial configuration prototype
Role Transport/utility helicopter
National origin Russia
Manufacturer Kamov
First flight 24 December 1998[1]
Number built 2[2]

The Kamov Ka-60 Kasatka (Russian: "Касатка": "Orca") is a Russian helicopter that first flew on 24 December 1998.

Design and development

File:Kamov Ka-60 Kasatka, Kamov AN2139086.jpg
Early configuration Ka-60 demonstrator at MAKS 2009

The Ka-60 has an estimated local military market of 200 units (Army aviation units, Border Police and Ministry of Internal Affairs).[citation needed] Intended as a replacement for the Mil Mi-8, the Ka-60 is to be used for aerial reconnaissance, for transporting air-assault forces, radio-electronic jamming, for special-operations missions and for various light-transport missions. Variations for foreign sale are expected. Manufacture is to take place at Ulan-Ude.

A civil version, the Ka-62, was initially proposed when the Ka-60 programme was launched, but no production followed owing to development problems with the Ka-60's Saturn RD-600V engines. Instead, an agreement was signed in April 2011 to use the 1,306 kW (1,751 hp) Turbomeca Ardiden 3G turboshaft for a revised Ka-62. A five-bladed main rotor will be driven via a new transmission, while the helicopter will have a revised cabin with larger windows and new avionics. First flight of the Ka-62 was planned for May 2013, with certification in 2014. Four prototypes and an initial batch of 16 Ka-62s for the Russian Ministry of Defence are currently planned,[3] and another 12 have been ordered for South America. It has a fantail, a 30-minute run-dry gearbox by Zoerkler, and can operate on one engine up to 9,500 ft (2,900m).[4]

Variants

File:Russian Air Force Ka-60.jpg
First Kamov Ka-60 demonstrator at MAKS 2003
  • Ka-60: Basic multi-role model.
  • Ka-60U: Training.
  • Ka-60K: Naval version.
  • Ka-60R: Reconnaissance.
  • Ka-62: New model for the civilian market. It has a redesigned fuselage with a high degree of composites, a larger cabin than the earlier demonstrators and will be equipped with Turbomeca Ardiden 3G engines.[5]
  • Ka-64 Sky Horse: Export model. Western certified, equipped with two General Electric T700/CT7-2D1 engines and five-blade main rotor.

Operators

 Russia
 Brazil
  • Atlas Taxi Aereo (7 on order)[8]
 Colombia

Specifications

Data from Jane's All The World's Aircraft 2003–2004,[1] Russian Helicopters[5]

General characteristics

  • Crew: 1-2
  • Capacity:
    • 12-15 passengers (Ka-62)
    • 14 infantry troops or 6 stretchers
    • Internal 2,000 kg (4,400 lb)
    • External 2,500 kg (5,500 lb)
  • Length: 15.60 m (51.2 ft)
  • Rotor diameter: 13.50 m (44.3 ft)
  • Height: 4.60 m (15.1 ft)
  • Disc area: 143.10 m² (1,540.3 sq ft)
  • Max. takeoff weight: 6,500 kg (14,300 lb)
  • Powerplant: 2 × Turbomeca Ardiden 3G turboshaft, 1,776 shp (1,324 kW) each

Performance

See also

Aircraft of comparable role, configuration and era
Related lists

References

  1. 1.0 1.1 Jackson 2003, pp. 373–374.
  2. Lua error in package.lua at line 80: module 'strict' not found.
  3. Butowski Air International September 2012, pp. 66–67.
  4. Mladenov, Alexander. "Kamov’s Six-Tonne Twin" Air International January 2014, page 74. Accessed: 17 June 2014.
  5. 5.0 5.1 Lua error in package.lua at line 80: module 'strict' not found.
  6. Kamov Ka-60, warfare.ru, Russian Military Analisis. Retrieved on September 8, 2008.
  7. Lua error in package.lua at line 80: module 'strict' not found.
  8. Lua error in package.lua at line 80: module 'strict' not found.
  9. Lua error in package.lua at line 80: module 'strict' not found.
  • Butowski, Piotr. "Russia's Resyled Helicopter". Air International, Vol. 82 No. 3. pp. 66–67. ISSN 0306-5634.
  • Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK:Jane's Information Group, 2003. ISBN 0-7106-2537-5.
  • "Nezavisimaya Gazeta", №241 (1812), 25 December 1998. translation

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