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| Technical data | ||
|---|---|---|---|
| Type | M-29 | ||
| Function | Passenger Airliner | ||
| Year | 1956 | ||
| Crew | See 201m | ||
| Engines | 4*9400kg VD-7 | ||
| Length | 47.5m | ||
| Wingspan | 53.0m | ||
| Tailplane span | 15.5m | ||
| Fuselage diameter | 4.2m | ||
| Wing area | m2 | ||
| Empty weight | kg | ||
| Loaded weight | kg | ||
| Wing load | kg/m2 | ||
| Power load | kg/hp | ||
| Trust-to-Weight | |||
| Speed at 0m | km/h | ||
| Speed at m | km/h | ||
| Landing Speed | km/h | ||
| Landing Roll | m sec | ||
| Takeoff Roll | m sec | ||
| Turn time | sec | ||
| Range | km | ||
| Flight Endurance | hmin | ||
| Ceiling | m | ||
| Climb | |||
| 1000m | min | ||
| 3000m | min | ||
| Payload | |||
| Seats | 200-250 | ||
| Load | kg | ||
| Created February 24, 1998
by Alexandre Savine and Sergey Andreev; |
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