Su-29, P.O.Sukhoj
T wo-seater, designated for aerobatic training, competitions and airshows. Aircraft is based on
Su-26M single-seater and utilizes most of technology of the predecessor. Thanks
to wider use of composite materials, aircraft performance with one pilot is similar to this of a single-seater predecessor.
| Technical data | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Type | Su-29 | |||||||||
| Function | Aerobatic trainer | |||||||||
| Year | 1992? | |||||||||
| Crew | 2 | |||||||||
| Engines | 1*360hp M-14P | |||||||||
| Length | m | |||||||||
| Wingspan | m | |||||||||
| Wing area | m2 | |||||||||
| Empty weight | 735kg | |||||||||
| Loaded weight | 862kg | |||||||||
| Maximum takeoff weight | 1200kg | |||||||||
| Wing load | kg/m2 | |||||||||
| Power load | 2.39kg/hp | |||||||||
| Maximum Speed (horizontal) | 325km/h | |||||||||
| Maximum allowed | 450km/h | |||||||||
| Landing Speed | 120km/h | |||||||||
| Landing Roll | m sec | |||||||||
| Takeoff Roll | m sec | |||||||||
| Turn time | sec | |||||||||
| Roll rate | 6rad/sec | |||||||||
| g-Limits | +12/-10 | |||||||||
| Ferry Range | 1200km | |||||||||
| Flight Endurance | hmin | |||||||||
| Ceiling | m | |||||||||
| Climb | ||||||||||
| Rate at 0m | 16 m/sec | |||||||||
| Payload | ||||||||||
| Fuel | kg | |||||||||
| Cost (approx) | 190,000USD | |||||||||
| Created December 10, 1996
Modified February 10, 1999 by Alexandre Savine |
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