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Kamov Ka-26The Kamov Ka-26 (NATO reporting name Hoodlum) was a Soviet light utility helicopter. Light utility helicopter. Most of the fuselage is rectangular, removable box. Two 325 hp Vedeneev M-14V-26 radials (Ka-26). Entered production in 1966. 850 built. Development with one engine: Ka-126. (All the Ka-26/126/128/226 are "Hoodlum"s) Variants - Ka-226-50 - 28-Dec-2001 passed ground tests at Kumertau production facility
Specifications (Ka-26) General characteristics - Crew: two
- Capacity: 6 passengers or 900 kg (1,980 lb) of cargo
- Length: 7.75 m (25 ft 5 in)
- Main rotor diameter: 2x 13.00 m (42 ft 8 in)
- Height: 4.05 m (13 ft 3 in)
- Main rotor area: 265.5 m² (2,856 ft²)
- Empty: 1,950 kg (4,290 lb)
- Loaded: 3,250 kg (7,150 lb)
- Maximum takeoff: kg ( lb)
- Powerplant: 2x Vedeneyev M-14V-26 radial engines, 239 kW (320 hp) each
Performance - Maximum speed: 160 km/h (100 mph)
- Range: 465 km (290 miles)
- Service ceiling: 3,000 m (9,840 ft)
- Rate of climb: m/min ( ft/min)
- Main rotor loading: 12 kg/m² (2.5 lb/ft²)
- Power/Mass: 0.15 kW/kg (0.09 hp/lb)
External links - http://www.kamov.ru/
- http://www.aviation.ru/Ka/#26
Related content Related development: Comparable aircraft: Designation sequence: Ka-20 - Ka-22 - Ka-25 - Ka-26 - Ka-27 - Ka-28 - Ka-29
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