Sukhoi Su-26
The Sukhoi Su-26 is a single-seater aerobatics plane from the former Soviet Union, powered by a single radial reciprocating engine. The Su-26 has mid-mounted straight wings and fixed landing gear, the main gear mounted on a solid titanium arc.
The Sukhoi Su-26 made its first flight in June 1984, the original four having a two-bladed prop. The production switched to the Su-26M, with refined tail surfaces and a German-made MTV-9 3-blade composite propeller. Further refinements were made, and the model won both the men's and women's team prizes at the 1986 World Aerobatics Championships. The modified Su-26M3 with the new M9F 430-hp engine dominated the 2003 and 2005 Aerobatic World Championships as well as the 2004 European Championships.
Specifications (Su-26)
Data from Air Races Datasheet,[1] Su-26, 29, 31 Specifications[2]
General characteristics
- Crew: 1
- Length: 6.83 m (22 ft 5 in)
- Wingspan: 7.80 m (25 ft 7 in)
- Height: 2.89 m (9 ft 6 in)
- Wing area: 11.83 m² (127 ft²)
- Empty weight: 736 kg (1,619 lb)
- Max. takeoff weight: 1,206 kg (2,653 lb)
- Powerplant: 1 × Vedeneyev M-14P radial engine, 270 kW (360 hp)
Performance
- Maximum speed: 450 km/h (281 mph)
- Cruise speed: 295 km/h (193 mph)
- Range: 800 km (500 mi)
- Service ceiling: 4,000 m (12,120 ft)
- Rate of climb: 18 m/s (3,543 ft/min)
- Load factor: -10g to 12g
See also
- Related development
- Aircraft of comparable role, configuration and era
References
External links
Media related to Sukhoi Su-26 at Wikimedia Commons
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