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Ka-27
A Russian Navy Ka-27SP (Helix D) helicopter flies past the flight deck of USS Belleau Wood (LHA-3) (not shown)
Role Anti-submarine helicopter
Manufacturer Kamov
First flight 24 December 1973[1]
Introduction 1982
Primary users Soviet Navy
Russian Navy
Ukrainian Navy
Indian Navy
Unit cost $1,500,000[2]
Developed from Kamov Ka-25
Variants Kamov Ka-31

The Kamov Ka-27 (NATO reporting name 'Helix') is a military helicopter developed for the Soviet Navy, and currently in service in Russia, Ukraine, Vietnam, South Korea, China, Taiwan and India. Variants include the Ka-29 assault transport, the Ka-28 downgraded export version, and the Ka-32 for civilian use.

Contents

[edit] Design and development

The helicopter was developed for ferrying and anti-submarine warfare. Design work began in 1970 and the first prototype flew in 1973. It was intended to replace the decade-old Kamov Ka-25, and is similar in appearance to its predecessor due to the requirements of fitting in the same hangar space. Like other Kamov military helicopters it has a co-axial rotor, removing the need for a tail rotor.

[edit] Variants

A Ka-27 assigned to the Russian destroyer Admiral Vinogradov (DDG 572) flies near the guided-missile cruiser USS Vella Gulf (CG 72) while conducting operations in the Gulf of Aden.
Ka-25-2
First prototype.
Ka-27K
Anti-submarine warfare prototype.
Ka-27PL
(Helix-A) Anti-submarine warfare helicopter.
Ka-27PS
(Helix-D) Search and rescue helicopter, ASW equipment removed and winch fitted.
Ka-27PV
Armed version of the Ka-27PS.
Ka-28
(Helix-A) Export version of the Ka-27Pl.
Ka-29TB
(Helix-B) Assault transport helicopter, with accommodation for two pilots and 16 troops.
Ka-29RLD
Airborne early warning, surface surveillance helicopter; later redesignated Ka-31.
Kamov Ka-32S of Omega Helicopters at Moscow Bykovo airfield in 2004
Ka-32A
Civil transport helicopter. Initial production version.
Ka-32A1
Fire fighting helicopter, equipped with a Bambi bucket.
Ka-32A2
Police version, equipped with two searchlights and a loudspeaker.
Ka-32A4
Special search and rescue, salvage and evacuation version.
Ka-32A7
Armed version developed from the Ka-27PS.
Ka-32A11BC
Canadian-certified version.
Ka-32A12
Swiss-registered and approved version.
KA-32C
Little-known custom version.
Ka-32M
Projected development with 1839kW TV3-117VMA-SB3 engines. Probably replaced by the Ka-32-10 project.
Ka-32S
(Helix-C) Maritime utility transport, search and rescue helicopter, fitted with an undernose radar.
Ka-32T
(Helix-C) Utility transport helicopter, with accommodation for Two crew and 16 passengers.
Ka-32K
Flying crane helicopter, fitted with a retractable gondola for a second pilot.

[edit] Operators

The Ka-27.
Ka-27 operators
Ka-32 A12 of Heliswiss

[edit] Military operators

 Algeria
 China
 India
 Russia
 Soviet Union
 Ukraine
 Vietnam
 Serbia
 South Korea

[edit] Civilian operators

 Canada
  • Vancouver Island Helicopters (VIH) operates 3 Ka-32 A11 BC helicopters (two of them lease to Taiwanese civilian operator (Sunrise airlines) from 2001 until now).
 Indonesia
  • Indonesia plan to buy the Ka-32 for non-military purposes (evacuation, search and rescue, cargo and firefighting) and for the Indonesian Police (Polisi Lintas Udara)[3]
 Iran
  • Iran plans to manufacture at least 50 Ka-32's under license in Iran.[4]
 Portugal
  • Ka-32 are used for non-military purposes only, mostly firefighting.
 Russia
  • Omega Helicopters operates the Ka-32S
 South Korea
  • Korean Forestry Service and Coast Guard operate 36 Ka-32s'
 Spain
 South Africa

Kamov Ka-32 firefighting in Cape Town, South Africa

Heliswiss Ka-32 installs digital-tv transmitter in Århus, Denmark
 Switzerland
 Taiwan
  • Sunrise Airlines Company operates 1 Ka-32A11BC helicopters (B-77999) for heavy lifting, leasing from Canada VIH company.
 Turkey
 United States

[edit] Specifications (Ka-27)

General characteristics

  • Crew: 1-3, plus 2-3 specialists
  • Length: 11.30 m (37 ft 1 in)
  • Rotor diameter: 15.80 m (51 ft 10 in)
  • Height: 5.50 m (18 ft 1 in)
  • Empty weight: 6,500 kg (14,300 lb)
  • Loaded weight: 11,000 kg (24,200 lb)
  • Useful load: 4,000 kg (8,800 lb)
  • Max takeoff weight: 12,000 kg (26,400 lb)
  • Powerplant: 2× Isotov turboshaft engines, 1,660 kW (2,225 shp) each

Performance

Armament

Ka-27

Ka-29TB

  • 1 × mobile forward firing GShG-7.62 minigun with 1800 rounds,
  • 1 × 30 mm 2A42 cannon with 250 rounds (flexible semi-rigid mount, optional/removable with ammunition carried in cabin)
  • four external hardpoints for bombs, rockets, gunpods, munitions dispensers, special four round missile launchers for the 9K114 Shturm
  • contrary to some reports the internal weapon load is not retained and is replaced by an armoured passenger compartment for up to sixteen troops

Avionics

[edit] See also

Related development

Comparable aircraft

Related lists

[edit] References

[edit] Notes

  1. ^ Taylor 1996, pp.316-317
  2. ^ Global Aircraft - Ka-27 Helix
  3. ^ ANGKASA No.07 Edisi April 2007 (page 17)
  4. ^ [1]

[edit] Bibliography

  • Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1 85733 1981 1. 

[edit] External links




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