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Sukhoi Su-38
Type of aircraft From Wikipedia, the free encyclopedia
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The Sukhoi Su-38 (Russian: Сухой Су-38) is a Russian agricultural aircraft, the first aircraft of this type to be designed and built by the Sukhoi Design Bureau civil aircraft section (Sukhoi Civil Aircraft (CJSC)).
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Design and development
Design originally began in 1993 as a development of the Sukhoi Su-29 aerobatic aircraft.[1][2] Development was suspended due to economic problems, and when restarted in 1998, the aircraft was redesigned, reducing the aircraft's size and replacing the originally planned M-14 radial engine with a LOM Praha 337S inline engine.[1][3] The first prototype made its maiden flight on 27 July 2001, with a second flying by June 2002.[1] As no users have yet[when?] expressed interest in the aircraft, the project is currently proceeding at a low pace.[citation needed]
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Specifications (Su-38L)
Data from Jane's All The World's Aircraft 2005–2006[1]
General characteristics
- Crew: 1
- Capacity: 500 L (132.1 US gal; 110.0 imp gal) chemical hopper
- Length: 8.1 m (26 ft 7 in)
- Wingspan: 11.53 m (37 ft 10 in)
- Height: 2.655 m (8 ft 9 in)
- Airfoil: TsAGI P-31Y (16%) [4]
- Gross weight: 1,200 kg (2,646 lb)
- Fuel capacity: 210 L (55 US gal; 46 imp gal) in two wing tanks
- Powerplant: 1 × LOM Praha M337S 6-cylinder air-cooled inverted in-line piston engine, 184 kW (247 hp)
- Propellers: 3-bladed LOM B-546 ground-adjustable propeller
Performance
- Maximum speed: 150–180 km/h (93–112 mph, 81–97 kn) operating speed
- Stall speed: 76 km/h (47 mph, 41 kn)
- Ferry range: 1,200 km (750 mi, 650 nmi) without spraybars
- 900 km (559 mi; 486 nmi) with spraybars fitted
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See also
Aircraft of comparable role, configuration, and era
References
Further reading
External links
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