| Date
| Model
| Comments
|
| September 25, 1929
| KaSkr-I Gyrocraft
| The first Soviet autogyro, designed by Kamov and Skrzhinskii. Based on Cierva models.
|
| 1934
| A-7
| An autogyro primarily used for observation duties.
|
| 1944
| Ka-8 Vertolet
| With his first true helicopter, Kamov introduced the coaxial scheme that the bureau still uses.
The Ka-8 was a single-seat helicopter with a 27 hp motorcycle engine, boosted to 45 hp by using alcohol for fuel.
The rotor blades were made of reinforced wood. Three units built.
|
| September 1949
| Ka-10 Hat
| The Hat was an improved Ka-8 with a 55 hp Ivchenko engine that can reach 90 km/h.
The twin - tail was introduced in the Ka-10M. 12 units built.
|
| 1952
| Ka-15 Hen
| A two-seat multi-purpose helicopter designed primarly for the Soviet Navy that became known outside the USSR in 1955.
The civilian version was the Ka-15M.
Engine: 1 Ivchenko of 225 hp Speed: 150 km/h Service Ceiling: 3050 m
|
| 1955
| Ka-18 Hog
| A Ka-15 with a large fuselage and a 280 hp Ivchenko AI-14VF engine. Could carry 4 passengers.
200 units built ( approx. )
|
| 1960
| Ka-20 Harp
| First seen in the Soviet National Aviation Day of 1961, it was considered the Ka-25 prototype.
Was very similar to the Ka-15 and Ka-18.
|
| 1960
| Ka-22 Hoop Vintokryl
| This convertiplane achieved several records but only one unit was produced.
October 14, 1961 : The Ka-22 reaches 337 km/h on 100 km circuit
|
| 1965
| Ka-25 Hormone
| Ship-borne helicopter for the Soviet Navy. Near 500 built up to 1975
Ka-25BSh Hormone - A : ASW variant
Ka-25OTH Hormone - B : Targeting variant for feeding guidance data to cruise missiles launched by surface warships and submarines
Ka-25PS Hormone - C : SAR variant
Ka-25K : Civilian Crane variant
Rotor diameter: 15.74 m Length: 10 m Height: 5.37 m Weight: 4770 kg - Max: 7500
Engine: 2 Glushenkov GTD-3F of 900 hp Speed: Max: 220 km/h Range: 400 km Service Ceiling: 3500 m
|
| 1966
| Ka-26 Hoodlum-A
| A typical Kamov design, a multi-purpose helicopter widely used by Aeroflot and exported to several countries.
More than 600 units built.
|
| 1969
| V-50
| An attack helicopter project with tandem rotors. Cancelled.
|
| 1978
| Ka-27 Helix
|
|
| 1981
| Ka-28 /
Ka-32 Helix
| Civilian derivative and export variants of the Ka-27
|
| July 27, 1982
| Ka-50 Hokum-A
| Also known as V-80, Werewolf & Black Shark
Ka-52 twin-seat Alligator
Ka-40 Hokum export variants
|
| 1986
| Ka-116 Hoodlum-B
| Turbine engine development of the Ka-26
|
| Middle of the 80s
| V-100
| A heavy attack helicopter project with a pusher propeller to exceed the speed of 400 km/h.
It was to be armed with 3000 kg of bombs/rockets, two guns, and two anti-radar/anti-ship missiles. Not built.
|
| 1990
| Ka-118
| A NOTAR ( No TAil Rotor ) development.
|
| 1993
| Ka-128
| A Ka-126 development with an added intermediate gearbox, and Bendix King avionics.
|
| 1994
| Ka-62
| Unique single main rotor operational helicopter by Kamov
|
| 1994
| Ka-226
| Twin engine development of the Ka-126
|
| 90s
| Ka-37
| An unmanned coaxial helicopter developed with Daewoo of South Korea initially designed for agricultural tasks.
Performances are a max weight of 250 kg ( 50 payload ), speed of 110km/h, and a flight duration about 45 minutes.
|