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Kamow KA-126

Further development of the Kamov Ka-26 that always suffered from a lack of power. With the Ka-126, this problem was solved by installing a single TVO-100 turbine. In view of the production problems with TVO-100 powerplants, there were plans to use a single Pratt & Whitney PT6B-36 powerplant with 716 shp. It is not known which alternative was chosen by Kamov.

Ka-126

Specifications

Version   KA-126
Dimensions
Overall length m 13,00
Overall height m 4,15
Fuselage length m 7,75
Main rotor diameter m 13,00
Masses
Max. take-off mass kg 3250
Empty mass kg  
Powerplant
Engine   1x Omsk TVO-100 Turbine
Max. turbine power kW 1x 536
Flight performance and limits
Max. speed km/h 180
Cruise speed km/h 160
Max. range km 650
Max. endurance h 4,5
Hover ceiling OGE m 1000
Service ceiling m 3850

Kamow KA-226

Further development of the Kamov Ka-126 with the single TVO-100 powerplant being replaced by two Allison 250 C20B shaft turbines.

KA-226_3V

Specifications

Version   KA-226
Dimensions
Overall length m 13,00
Overall height m 4,15
Fuselage length m 8,10
Main rotor diameter m 13,00
Masses
Max. take-off mass kg 3400
Empty mass kg  
Powerplant
Engine   2x Allison 250 C20B
Max. turbine power kW 2x 313
Flight performance and limits
Max. speed km/h 205
Cruise speed km/h 185
Max. climb rate m/s -
Max. range km 650
Max. endurance h -
Hover ceiling (IGE) m -
Hover ceiling (OGE) m 1950
Service ceiling m 5250

Kamow KA-50 Werewolf

Type: Attack helicopter
Crew: 1
Rotor unit: Coaxial, 2x 3 rotor blades
Undercarriage: Wheel, front 1 (twin), rear 2, retractable
Versions: Prototype V-80, Ka-52
Coverage: Russia, Slovakia (planned)
Armament: 1x 30mm 2A42 cannon; optional: 80mm fire-and-forget missiles, AT-9 Whirlwind anti-tank missiles, ASMs, short-range AAMs (anti-aircraft missiles)
Notes: Competing helicopter against the Mil Mi-28; further development is the Ka-52 Alligator with parallel cockpit

Specifications

Version   KA-50
Dimensions
Overall length m 16,0
Overall height m 5,40
Fuselage length m  
Main rotor diameter m 2x 14,5
Masses
Max. take-off mass kg 10800
Empty mass kg  
Powerplant
Engine:   2x Klimow Tw3-117VK
Max. turbine power kW 2x 1640
Flight performance and limits
Max. speed km/h 350
Cruise speed km/h  
Max. climb rate m/s Approx. 10
Max. range km Approx. 500
Max. endurance h  
Hover ceiling (IGE) m  
Hover ceiling (OGE) m 4000
Service ceiling m  

Kamow KA-52 Alligator

Type Combat / command helicopter
Crew 2
Rotor unit Coaxial, 2x 3 rotor blades
Undercarriage Wheel, front 1, rear 2, retractable

Ka-52

Specifications

Version   KA-52
Dimensions
Overall length m 16,0
Overall height m 4,95
Fuselage length m 13,53
Main rotor diameter m 2x 14,5
Masses
Max. take-off mass kg  
Empty mass kg  
Powerplant
Engine   2x Klimow Tw3-117VK
Max. turbine power kW 2x 1640
Flight performance and limits
Max. speed km/h  
Cruise speed km/h  
Max. climb rate m/s  
Max. range km  
Max. endurance h  
Hover ceiling (IGE) m  
Hover ceiling (OGE) m  
Service ceiling m  

Kamow KA-62

The Kamov Ka-62 is a multi-purpose helicopter of the 6-to class. It can carry up to 16 passengers or 2,000 kg. It represents a deviation from the classical coaxial design of the Kamov helicopters and is targeting the western market.Ka-62

Specifications

Version   KA-62
Dimensions
Overall length m  
Overall height m 3,70
Fuselage length m 12,80
Main rotor diameter m 13,00
Masses
Max. take-off mass kg Approx. 6,000
Empty mass kg Approx. 4,000
Powerplant
Engine   2x RD-600
Max. turbine power kW 2x 1300
Flight performance and limits
Max. speed km/h 300
Cruise speed km/h 270
Max. range km 600
Max. climb rate m/s Approx. 12
Max. hover ceiling (OGE) m 2000
Service ceiling m 5500

Kamow V-50

Type Design for an attack helicopter
Crew 3
Rotor unit Tandem, 2x 3 rotor blades
Undercarriage Wheel, front 2, rear 2

Kamow V-50

By courtesy of Peter Wernli
(from "Die Hubschrauber-Industrien Russlands & Polens" by Peter Wernli)

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