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M eteorological observation aircraft. Specially modified for atmospheric, geophysical, high
elevation observations at mountain ranges. Engine performance was boosted by TK-9 turbocharger, providing 850hp up to
9500m altitude.
| Technical data | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Type | An-6 | |||||||||
| Function | Meteo observation | |||||||||
| Year | 1948 | |||||||||
| Crew | 2+1 | |||||||||
| Engines | 1*1000/850hp turbocharged ASh-62IR | |||||||||
| Length | 13.2m | |||||||||
| Wingspan | 18.18m | |||||||||
| Wing area | 71.5m2 | |||||||||
| Empty weight | 3540kg | |||||||||
| Loaded weight | 5250kg | |||||||||
| Wing load | 73.5kg/m2 | |||||||||
| Power load | 5.2kg/hp | |||||||||
| Speed at ?m | 280km/h | |||||||||
| Landing Speed | 85km/h | |||||||||
| Landing Roll | 170m | |||||||||
| Takeoff Roll | 180m | |||||||||
| Flight Endurance | 4h | |||||||||
| Ceiling | 11000m | |||||||||
| Created January 25, 1996
Modified September 10, 1998 by Alexandre Savine |
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