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Length |
6.90 m |
Height |
2.00 m |
Wing span |
7.80 m |
Wing area |
11.83 m² |
Engine |
M14 P, 9-cylinder 4-stroke, gasoline, air-cooled |
Horse power |
360 - 420 HP |
Propeller |
Mühlbauer 3-blade composite |
Construction |
Carbon Fiber, steel titanium |
Fuel |
Gasoline 100LL (AVGAS) |
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Empty Weight |
680 kg |
Maximum aerobatic weight (A)
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810 kg |
Maximum take off weight (N)
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850 kg |
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Load Factor |
+10g /-10g |
Max. allowed speed |
450 km/h |
Max. cruising speed |
220 km/h |
Max. roll rate |
400°/sec |
Max. rate of climb |
18 m/sec. |
Take-off run
(brake release to lift off)
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125 m |
Take - off to 15 m
(brake release to 15 m height) |
280 m |
Landing distance over 15 m
(15 m height to stop) |
380 m |
Landing roll
(touch down to stop) |
280 m |
Touchdown speed |
125 km/h |
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Sukhoi
Design Bureau, Russia |
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© 1996-2018 Jean-Louis Monnet. All Rights Reserved
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