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Sukhoi Su-29

Aerobatic and sport aircraft built in Russia From Wikipedia, the free encyclopedia

Sukhoi Su-29
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The Sukhoi Su-29 is a Russian two-seat aerobatic aircraft with a 268 kW (360 hp) radial engine. It was designed based on the Su-26 and inherited most of the design and technical features of its predecessor. Due to wide use of composite materials, which make up as much as 60% of the Su-29's aircraft structure, the empty weight is increased by only 50 kg (110 lb) over the single-seat Su-26's empty weight.

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The Su-29 is used for initial pilot aerobatics education, flight training, and participation of pilots in aerobatics competitions and air shows, as well as for maintaining flight skills of military and civil pilots.

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Operators

Argentina
Austria
  • Flying Bulls
 Canada
Czechia
  • Czech aerobatic team
Russia

Specifications (Su-29)

Data from Jane's All The World's Aircraft 1993–94,[5] Sukhoi[6]

General characteristics

  • Crew: 2
  • Length: 7.29 m (23 ft 11 in)
  • Wingspan: 8.2 m (26 ft 11 in)
  • Height: 2.87 m (9 ft 5 in)
  • Wing area: 12.24 m2 (131.8 sq ft)
  • Airfoil: root: Symmetrical 18% ; tip: Symmetrical 12%[7]
  • Empty weight: 760 kg (1,676 lb)
  • Max takeoff weight: 1,100 kg (2,425 lb)
  • Powerplant: 1 × Vedeneyev M14P 9-cylinder air-cooled radial piston engine, 265 kW (355 hp)
  • Propellers: 3-bladed, 2.4 m (7 ft 10 in) diameter

Performance

  • Maximum speed: 340 km/h (210 mph, 180 kn)
  • Cruise speed: 295 km/h (183 mph, 159 kn)
  • Stall speed: 110 km/h (68 mph, 59 kn)
  • Ferry range: 965 km (600 mi, 521 nmi)
  • Service ceiling: 4,000 m (13,000 ft)
  • g limits: +12
  • Roll rate: >360°/s
  • Rate of climb: 18 m/s (3,500 ft/min)
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See also

Related development

Aircraft of comparable role, configuration, and era

References

Further reading

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