||It has been suggested that Kamov V-60 be merged into this article. (Discuss) Proposed since December 2013.|
|Manufacturer||Industria Aeronautică Română|
|First flight||22 December 1988|
|Developed from||Kamov Ka-26|
|Developed into||Kamov Ka-226|
The Kamov Ka-126 (NATO reporting name Hoodlum) is a Soviet light utility helicopter with co-axial rotors. Evolved from Ka-26 with engine pods removed from stub wings, fitted with one TVO-100 turboshaft engine positioned on top of fuselage, modified rotor blades, new fuel system.
Development began 1984 with the signing of governmental Romanian-Soviet agreement in the field of aeronautical construction for cooperation in manufacturing a utility helicopter derived from Kamov Ka-26 helicopter.In October 1985 the signing of the collaboration protocol for the manufacturing of the single engine turbine powered KA 126 helicopter. In 1986 Industria Aeronautică Română(IAR) starts the helicopter manufacturing preparation. Early mockup had two small turboshafts above cabin; single turboshaft adopted subsequently; ground test vehicle completed early 1986; On 22 December 1988 was maiden flight of the IAR Built Ka 126 with TV100 engine produced by Turbomecanica București and VR126 main gear built by I. Avioane Bacău today Aerostar. After building 17 Ka 126 production was stopped and after 1991 the program was cancelled.
- A twin engine variant was developed as the Ka-226.
All the Ka-26/126/128/226 variants are codenamed "Hoodlum".
The fuselage of the Ka-126 consists of a fixed, bubble-shaped cockpit containing the pilot and co-pilot, plus a removable, variable box available in medevac, passenger-carrying and cropduster versions. The helicopter can fly with or without the box attached, giving it much flexibility in use.
- Ka-126 Hoodlum-B
- One or two crew utility light helicopter, powered by a 720-shp (537-kW) (Glushenkov) OMKB TVD-100 turboshaft engines. First flown in 1986, and built under licence by IAR in Romania. 2 prototypes and 15 series helicopter built.
- Kamov V-60
- A proposed light armed escort helicopter based on the Ka-126.
- One prototype, powered by a 722-shp (538-kW) Turbomeca Arriel 1D1 turboshaft engine.
- Kamov Ka-226
- Powered by two 450-shp (335-kW) Rolls-Royce 250-C20R/2 turboshaft engines.
Data from Jane's All The World's Aircraft 1993–94
- Crew: 2
- Capacity: 6 passengers (cargo/passenger pod)
- Payload: 1,000 kg (2,205 lb) (slung load) or 1000 L (220 Imp Gallons) chemical hopper
- Length: 7.775 m (25 ft 6 in)
- Rotor diameter: 13.00 m (42 ft 7¾ in)
- Height: 4.155 m (13 ft 7½ in)
- Disc area: 265.5 m² (2,856 ft²)
- Empty weight: 1,915 kg (4,222 lb)
- Max. takeoff weight: 3,250 kg (7,165 lb)
- Powerplant: 1 × Omsk TVO-100 turboshaft, 522 kW (700 hp)
- Maximum speed: 180 km/h (97 knots, 112 mph)
- Cruise speed: 160 km/h (86 knots, 99 mph)
- Range: 713 km (384 nmi, 443 mi)
- Endurance: 5 hr 36 min
- Service ceiling: 3,850 m (12,630 ft)
- Rate of climb: 6.6 m/s (1,300 ft/min)
- Related development
- Aircraft of comparable role, configuration and era
- Lambert 1993, pp. 277–278.
- Lambert, Mark. Jane's All The World's Aircraft 1993–94. Coulsdon, UK: Jane's Data Division, 1993. ISBN 0-7106-1066-1.
- R. Simpson "Airlife's Helicopter and Rotorcraft", 1998
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