| Technical data | |
|---|---|
| Type | Su-39 |
| Function | trainer |
| Year | 2001? |
| Crew | 2 |
| Engines | 1*400hp Vedeneyev M-14PF or 1*360hp Vedeneyev M-14P |
| Length | 7.28m |
| Height | 2.60m |
| Wingspan | 8.5m |
| Wing area | 12.2m2 |
| Empty weight | 850kg |
| Loaded weight | 1300kg |
| Wing Load (kg/m2) | 107 |
| Power load (kg/hp) | 3.6 |
| Maximum Speed | 370km/h |
| Dynamic load | +11-8g |
| Landing Speed | 110km/h |
| Landing Roll | 350m |
| Takeoff Roll | 230m |
| Range | 1500km |
| Fuel consumption | 17g/km |
| Ceiling | 7000m |
| Climb | |
| at 0m | 13.5m/sec |
| Payload | |
| Fuel | 260kg |
| Cargo | ?kg |
Primary trainer, designed to replace the Yak-52. Intended for training and skill maintaining of civil pilots and airforce cadets. Suitable also for airclubs, liaison and light transport duties.
The Su-39 is a tandem two seat aircraft with retractable tricycle landing gear, derived from the Su-26 and Su-29 aerobatic competition aircraft. Originally planned 400hp M-14PF engine was found unreliable and short on resource, and classic well-tested 360hp M-14P was fitted. Variety of navigation equipment may be custom-fitted, including GPS, long-range and short-range navigation and even automatic landing approach.
Expected resource is 10000hours. Airframe strength and power load allow to perform aerobatics in loads range +11/-10g. Both seats are equipped with SKS-94 emergency ejection system (same as on Su-31), developed by AOOT 'Zvezda', creator of the K-36 combat aircraft 0-0 ejection seat. Cost of one hour is 2 to 2.5 times less than for class aircraft in the other same.
Note that the recent upgrade of Su-25 attack plane is also designated Su-39. May be for confusion? See Su-39;
| Created December 10, 1996
Modified June 28, 1999 |
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